Polyethylene compositions, methods of making the same, and articles prepared therefrom

Information

  • Patent Grant
  • 8318862
  • Patent Number
    8,318,862
  • Date Filed
    Friday, October 19, 2007
    16 years ago
  • Date Issued
    Tuesday, November 27, 2012
    11 years ago
Abstract
The invention is related to films formed from a composition, comprising a blend, wherein said blend comprises a high molecular weight ethylene-based interpolymer and a low molecular weight ethylene-based interpolymer, and the high molecular weight ethylene-based interpolymer is a heterogeneously branched linear or a homogeneously branched linear ethylene-based interpolymer, and has a density from 0.922 g/cc to 0.929 g/cc, and a high load melt index (I21) from 0.2 g/10 min to 1.0 g/10 min, and the low molecular weight ethylene-based interpolymer is heterogeneously branched linear or a homogeneously branched linear ethylene-based interpolymer, and has a density from 0.940 g/cc to 0.955 g/cc, and a melt index (I2) from 6 g/10 min to 50 g/10 min. The blend has a single peak in an ATREF profile eluting above 30° C., and has a coefficient of viscosity average molecular weight (CMv) less than −0.0032 in the log(calculated Mv) versus elution temperature, said CMv calculated in the range of elution temperatures from 70° C. to 90° C. The Mv is the viscosity average molecular weight.
Description

The present invention provides films formed from polyethylene compositions, and articles formed from such films.


Polyethylene compositions with a multimodal molecular weight distribution (MWD), for example a bimodal MWD, can offer distinct advantages compared with unimodal polyethylenes or other polyolefins, in various applications, including film, pipe, and drip tape and tubing applications. Some multimodal polyethylenes compositions are described in the following International Publications: WO 03/020821; WO 03/102075; WO 97/29152; WO 00/01765; WO 00/18814; WO 01/02480; WO 01/25328; WO03/051937; WO03/033586; WO00/40620; U.S. Pat. No. 6,248,831; Japanese Publication Nos. 2004-217802 (Abstract); 2004-231844 (Abstract); 2003-253063 (Abstract); 2003-128848 (Abstract); 08-134285 (Abstract); and EP0492656B1.


Polyethylene films should have at least the following characteristics: (1) good dart impact, (2) good tear resistance, and (3) excellent stabilization against thermal and oxidative degradation during fabrication, and end use applications. These needs are particularly pronounced in shipping sack applications, such as heavy duty shipping sacks. There is also a need for a polyethylene film resin, which offers an advantageously balanced combination of thermal, mechanical, and processing properties. In particular, there is a need for film resins that exhibit an improved balance of extrudability, bubble stability, dart drop, tensile and tear properties, and FAR (Film Appearance Rating), while being able to be successfully extruded at all commercially required line speeds. Some of these needs and others have been met by the following invention.


SUMMARY OF THE INVENTION

The invention provides a film comprising at least one component formed from a composition, comprising a blend, wherein said blend comprises a high molecular weight ethylene-based interpolymer and a low molecular weight ethylene-based interpolymer, and


wherein the high molecular weight ethylene-based interpolymer is a heterogeneously branched linear or a homogeneously branched linear ethylene-based interpolymer, and has a density from 0.922 g/cc to 0.929 g/cc, and a high load melt index (I21) from 0.2 g/10 min to 1.0 g/10 min, and


wherein the low molecular weight ethylene-based interpolymer is a heterogeneously branched linear or a homogeneously branched linear ethylene-based interpolymer, and has a density from 0.940 g/cc to 0.955 g/cc, and a melt index (I2) from 6 g/10 min to 50 g/10 min; and


wherein the blend has a single peak in an ATREF profile eluting above 30° C., and has a coefficient of viscosity average molecular weight (CMv) less than −0.0032 in the log(calculated Mv) versus elution temperature, said CMv calculated in the range of elution temperatures from 70° C. to 90° C., and wherein Mv is the viscosity average molecular weight.


The invention also provides for articles, each comprising at least one component formed from an inventive film as described herein.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 depicts ATREF-DV profiles of several blends and competitive resins.



FIGS. 2-29, each depicts an ATREF-DV overlay profile for one blend or competitive resin.





DETAILED DESCRIPTION OF THE INVENTION

The invention provides for a film comprising at least one component formed from a composition comprising a blend of ethylene-based interpolymers, in which the comonomer and molecular weight distribution are adjusted to provide a final blend, which shows a single peak in an ATREF profile eluting above 30° C., and which has a coefficient of viscosity average molecular weight (CMv) less than −0.0032 in the log(calculated Mv) versus elution temperature, said CMv calculated in the range of elution temperatures from 70° C. to 90° C. Here Mv is the viscosity average molecular weight.


The inventive compositions have several potential uses, including, but not limited to, films and sheets, as discussed above, and drip tape for agricultural use, and geomembranes. In addition, the inventive compositions can be azide modified to form articles of manufacture, such as geomembranes, with better sag and SCG resistance, over conventional Cr based resins.


As discussed above, the invention provides a film comprising at least one component formed from a composition, comprising a blend, wherein said blend comprises a high molecular weight ethylene-based interpolymer and a low molecular weight ethylene-based interpolymer, and


wherein the high molecular weight ethylene-based interpolymer is a linear interpolymer, and preferably, a heterogeneously branched linear or a homogeneously branched linear ethylene-based interpolymer, and has a density from 0.922 g/cc to 0.929 g/cc, and a high load melt index (I21) from 0.2 g/10 min to 1.0 g/10 min, and


wherein the low molecular weight ethylene-based interpolymer is a linear interpolymer, and preferably a heterogeneously branched linear or a homogeneously branched linear ethylene-based interpolymer, and has a density from 0.940 g/cc to 0.955 g/cc, and a melt index (I2) from 6 g/10 min to 50 g/10 min; and


wherein the blend has a single peak in an ATREF profile eluting above 30° C., and has a coefficient of viscosity average molecular weight (CMv) less than −0.0032 in the log(calculated Mv) versus elution temperature, said CMv calculated in the range of elution temperatures from 70° C. to 90° C., and wherein Mv is the viscosity average molecular weight. In a further embodiment, the blend is an in-situ blend.


In one embodiment, the high molecular weight ethylene-based interpolymer is present in an amount from 45 to 55 weight percent, based on the sum weight (calculated split %) of the high molecular weight ethylene-based interpolymer and the low molecular weight ethylene-based interpolymer.


In another embodiment, the high molecular weight ethylene-based interpolymer is a heterogeneously branched linear ethylene-based interpolymer.


In another embodiment, the low molecular weight ethylene-based interpolymer is a heterogeneously branched linear ethylene-based interpolymer.


In another embodiment, the high molecular weight ethylene-based interpolymer is a heterogeneously branched linear ethylene-based interpolymer, and the low molecular weight ethylene-based interpolymer is a heterogeneously branched linear ethylene-based interpolymer.


In another embodiment, the high molecular weight ethylene-based interpolymer has a density from 0.9229 g/cc to 0.9271 g/cc.


In another embodiment, the CMv is less than −0.0036. In another embodiment, the CMv is less than −0.0040. In another embodiment, the CMv is less than −0.0090.


In another embodiment, the composition has a density from 0.930 g/cc to 0.945 g/cc. In another embodiment, the composition has a density less than 0.945 g/cc. In another embodiment, the composition has a density less than, or equal to, 0.942 g/cc.


In another embodiment, the low molecular weight ethylene-based interpolymer has a melt index (I2) from 10 g/10 min to 40 g/10 min. In another embodiment, the low molecular weight ethylene-based interpolymer has a melt index (I2) from 15 g/10 min to 35 g/10 min.


In another embodiment, the composition has a melt index, I2, from 0.15 to 0.8 g/10 min, and a density greater than 0.9375 g/cc. In another embodiment, the composition has a melt index, I2, from 0.4 to 0.8 g/10 min.


In another embodiment, the low molecular weight ethylene-based interpolymer has a density less than 0.955 g/cc. In another embodiment, the low molecular weight ethylene-based interpolymer has a density less than 0.954 g/cc. In another embodiment, the low molecular weight ethylene-based interpolymer has a density less than 0.953 g/cc. In another embodiment, the low molecular weight ethylene-based interpolymer has a density less than 0.950 g/cc. In certain embodiments, the density of the low molecular weight component may be up to 0.957 g/cc.


In another embodiment, the composition has a melt index, I2, from 0.05 g/10 min to 0.5 g/10 min. In yet another embodiment, the composition has an I21/I2 ratio from 30 to 80. In a further embodiment, the composition has an I21/I2 ratio from 40 to 75 or from 45 to 75.


In another embodiment, the blend has less than 0.5 vinyls/1000 carbon, preferably less than 0.4 vinyls/1000 carbon, and more preferably less than 0.3 vinyls/1000 carbon.


In another embodiment, the high molecular weight ethylene-based interpolymer has a g′ value of one or greater.


In yet another embodiment, the high molecular weight ethylene-based interpolymer is an ethylene/α-olefin interpolymer. In a further embodiment, the α-olefin is selected from the group consisting of C3 to C10 α-olefins. In yet a further embodiment, the α-olefin is preferably propylene, 1-butene, 1-pentene, 1-hexene, 1-heptene, 1-octene, 1-nonene and 1-decene, and more preferably propylene, 1-butene, 1-hexene and 1-octene, and even more preferably 1-hexene.


In another embodiment, the low molecular weight ethylene-based interpolymer is an ethylene/α-olefin interpolymer. In a further embodiment, the α-olefin is selected from the group consisting of C3 to C10 α-olefins. In yet a further embodiment, the α-olefin is selected from the group consisting propylene, 1-butene, 1-pentene, 1-hexene, 1-heptene, 1-octene, 1-nonene and 1-decene, and more preferably propylene, 1-butene, 1-hexene and 1-octene, and even more preferably 1-hexene.


In another embodiment, the composition further comprising one or more additives. In a further embodiment, the one or more additives are selected from the group consisting of hindered amines, hindered phenols, metal deactivators, UV absorbers, phosphites, acid neutralizers, processing aids, and combinations thereof. In another embodiment, the one or more additives are selected from the group consisting of Cyasorb 3529, Irganox 1010, Irganox 1076, Irganox 1330, Irganox MD1024, Irgafos 168, calcium stearate, Dynamar FX 5911, and combinations thereof. In another embodiment, the one or more additives are selected from the group consisting of Cyasorb 3529, Irganox 1010, Irganox 1076, Irganox 1330, Irganox MD1024, Doverphos 9228, calcium stearate, Dynamar FX 5911, and combination thereof. In another embodiment, the one or more additives are selected from the group consisting of UV N30, Irganox 1330, Doverphos 9228, Irganox MD1024, HO3, calcium stearate, Dynamar FX 5911, and combinations thereof.


An inventive film may be formed from a composition that comprises a combination of two or more embodiments as described herein.


In another embodiment, the film is a multi-layered film. In another embodiment, the film is a single layered film. In yet another embodiment, the film has a thickness from 2 mils to 50 mils, preferably from 3 mils to 30 mils, and more preferably from 4 mils to 20 mils. In another embodiment, the film has a thickness from 1 mil to 100 mils.


In another embodiment, an inventive film is formed using a blown film process. In another embodiment, an inventive film is formed using a cast film process.


The invention also provides a sheet comprising at least one component formed from an inventive film as described herein. In a further embodiment, the sheet has a thickness from 2 mils to 200 mils, preferably from 10 mils to 150 mils, and more preferably from 20 mils to 100 mils. In another embodiment, the sheet has a thickness from 2 mils to 500 mils.


In another embodiment, the sheet is formed using a blown film process. In another embodiment, the sheet is formed using a cast film process.


In another embodiment, the film has an Elmendorf Tear Strength, in the machine direction (MD), greater than, or equal to, 100 g/mil, preferably greater than, or equal to, 120 g/mil, and more preferably greater than, or equal to 140 g/mil.


In another embodiment, the film has an Elmendorf Tear Strength, in the traverse direction (TD), greater than, or equal to, 220 g/mil, preferably greater than, or equal to, 240 g/mil, and more preferably greater than, or equal to 260 g/mil.


In another embodiment, the film has a Normalized Dart Impact (B scale) greater than, or equal to, 60 grams, preferably greater than, or equal to, 80 grams, and more preferably greater than, or equal to 100 grams.


An inventive film may comprise a combination of two or more embodiments as described herein.


The invention also provides an article comprising at least one component formed from an inventive film. In one embodiment, the article is a shipping sack. In another embodiment, the article is a geomembrane. In another embodiment, the article is a drip tape (for example an agricultural tape).


An inventive article may comprise a combination of two or more embodiments as described herein.


Polymer Composition


As discussed above, the inventive compositions comprise a blend containing a high molecular weight ethylene-based interpolymer and a low molecular weight polyethylene-based interpolymer. Additional features of these components are described below.


The High Molecular Weight (HMW) Component


The high molecular weight ethylene-based interpolymer has a density greater than, or equal to, 0.922 g/cc, preferably greater than, or equal to, 0.9225 g/cc, and more preferably greater than, or equal to, 0.923 g/cc. In another embodiment, the high molecular weight ethylene-based interpolymer has a density less than, or equal to, 0.929 g/cc, preferably less than, or equal to, 0.928 g/cc, and more preferably less than, or equal to 0.927 g/cc. In another embodiment, the density of the high molecular weight ethylene-based interpolymer is in the range from 0.922 to 0.928 g/cc, and preferably in the range from 0.9229 to 0.9271 g/cc.


The high molecular weight ethylene-based interpolymer has a high load melt index, I21, (190° C., 21.6 kg weight, ASTM 1238-03) greater than, or equal to, 0.20, preferably greater than, or equal to, 0.25, and more preferably greater than, or equal to, 0.30 (units of grams per 10 minutes). In another embodiment, the high molecular weight ethylene-based interpolymer has a high load melt index, I21 less than, or equal to, 1.0, preferably less than, or equal to, 0.9, and more preferably less than, or equal to, 0.8. In yet another embodiment, the I21 ranges from 0.20 to 1.0 grams per 10 minutes, and preferably from 0.25 to about 1.0 grams per 10 minutes.


In another embodiment, the high molecular weight ethylene-based interpolymer is an ethylene/α-olefin interpolymer. In a preferred embodiment, the α-olefin is a C3-C20 α-olefin, a C4-C20 α-olefin, and more preferably a C4-C12 α-olefin, and even more preferably a C4-C8 α-olefin, and most preferably C6-C8 α-olefin.


The term “interpolymer,” as used herein, refers to a polymer having polymerized therein at least two monomers. It includes, for example, copolymers, terpolymers and tetrapolymers. As discussed above, it particularly includes a polymer prepared by polymerizing ethylene with at least one comonomer, typically an alpha olefin (α-olefin) of 3 to 20 carbon atoms (C3-C20), or 4 to 20 carbon atoms (C4-C20), or 4 to 12 carbon atoms (C4-C12) or 4 to 8 carbon atoms (C4-C8), or 6 to 8 carbon atoms (C6-C8). The α-olefins include, but are not limited to, propylene 1-butene, 1-pentene, 1-hexene, 4-methyl-1-pentene, 1-heptene, and 1-octene. Preferred α-olefins include propylene, 1-butene, 1-pentene, 1-hexene, 4-methyl-1-pentene, 1-heptene, and 1-octene. Especially preferred α-olefins include 1-hexene and 1-octene, and more preferably 1-hexene. The α-olefin is desirably a C3C10 α-olefin, and more desirably a C3C8 α-olefin, and most desirably C6-C8 α-olefin.


Interpolymers include ethylene/butene (EB) copolymers, ethylene/hexene-1 (EH), ethylene/octene-1 (EO) copolymers, ethylene/alpha-olefin/diene modified (EAODM) interpolymers such as ethylene/propylene/diene modified (EPDM) interpolymers and ethylene/propylene/octene terpolymers. Preferred copolymers include EB, EH and EO copolymers, and most preferably EH and EO copolymers.


In a preferred embodiment, the high molecular weight ethylene-based interpolymer is an ethylene/1-hexene interpolymer. In a further embodiment, the ethylene/1-hexene copolymer has a hexene/ethylene (C6/C2) ratio from 0.03:1 to 0.105:1. In yet a further embodiment, the ethylene/1-hexene copolymer has a hydrogen/ethylene (H2/C2) ratio from 0.01 to 0.09. In another embodiment, the high molecular weight ethylene-based interpolymer has a g′ of 1 signifying a linear polymer.


The high molecular weight component may comprise a combination of two or more embodiments as described herein.


The Low Molecular Weight (LMW) Component


The low molecular weight ethylene-based interpolymer has a density greater than, or equal to, 0.940 g/cc, preferably greater than, or equal to, 0.942 g/cc, and more preferably greater than, or equal to, 0.945 g/cc. In another embodiment, the low molecular weight ethylene-based interpolymer has a density less than, or equal to, 0.957 g/cc, preferably less than, or equal to, 0.955 g/cc. In another embodiment, the low molecular weight ethylene-based interpolymer has a density less than, or equal to, 0.953 g/cc. In another embodiment, the density ranges from 0.940 to 0.955 g/cc, and preferably from 0.946 to 0.955 g/cc.


The low molecular weight ethylene-based interpolymer has a melt index, I2, (190° C., 2.16 kg weight, ASTM 1238-03) greater than, or equal to, 6, preferably greater than, or equal to, 7, and more preferably greater than, or equal to, 8 (units of grams per 10 minutes). In another embodiment, the low molecular weight ethylene-based interpolymer has a melt index, I2, less than, or equal to, 50, preferably less than, or equal to, 47, and more preferably less than, or equal to, 45. In another embodiment, the melt index range from 6 to 50 grams per 10 minutes, preferably in the range from 8 to 47 grams per 10 minutes, more preferably in the range from 10 to 45 grams per 10 minutes, and even more preferably from 15 to 25 grams per 10 minutes.


In another embodiment, the low molecular weight ethylene-based interpolymer is an ethylene/α-olefin interpolymer. In another embodiment, the α-olefin is a C3-C20 α-olefin, a preferably a C4-C20 α-olefin, and more preferably a C4-C12 α-olefin, and even more preferably a C4-C8 α-olefin and most preferably C6-C8 α-olefin. The α-olefins include, but are not limited to, propylene 1-butene, 1-pentene, 1-hexene, 4-methyl-1-pentene, 1-heptene, and 1-octene. Preferred α-olefins include propylene, 1-butene, 1-pentene, 1-hexene, 4-methyl-1-pentene, 1-heptene, and 1-octene. Especially preferred α-olefins include 1-hexene and 1-octene, and more preferably 1-hexene. The α-olefin is desirably a C3-C8 α-olefin, and more desirably a C4-C8 α-olefin and most desirably a C6-C8 α-olefin.


Interpolymers include ethylene/butene-1 (EB) copolymers, ethylene/hexene-1 (EH), ethylene/octene-1 (EO) copolymers, ethylene/alpha-olefin/diene modified (EAODM) interpolymers such as ethylene/propylene/diene modified (EPDM) interpolymers and ethylene/propylene/octene terpolymers. Preferred copolymers include EB, EH and EO copolymers, and most preferred copolymers are EH and EO.


In a preferred embodiment, the low molecular weight component is an ethylene/1-hexene copolymer. In a further embodiment, the ethylene/1-hexene copolymer has a hexene/ethylene (C6/C2) ratio from 0.01 to 0.065. In yet a further embodiment, the ethylene/1-hexene copolymer has a hydrogen/ethylene (H2/C2) ratio from 0.1 to 1.0. The LMW component is a linear polymer.


The low molecular weight component may comprise a combination of two or more embodiments as described herein.


In a preferred embodiment, the LMW component is determined by operating at a known set of reactor conditions to produce the desired component melt index and density. These conditions are determined by producing that product alone to determine the appropriate reactor temperature, H2/C2 and C6/C2 ratios, which are then used when operating the LMW component, as the second reactor, in series, to produced the desired Melt Index and Density.


One preferred process for producing the LMW component alone is as follows. Ethylene is copolymerized with 1-hexene in a fluidized bed reactor. The polymerization is continuously conducted after equilibrium is reached, under the respective conditions, as set forth in the tables (see Tables 1A and 1B) below. Polymerization is initiated by continuously feeding the catalyst and cocatalyst into a fluidized bed of polyethylene granules, together with ethylene, 1-hexene and hydrogen. Inert gases, nitrogen and isopentane, make up the remaining pressure in the reactors. A model of this data could then be developed, and used to control this second reactor component.









TABLE 1A







Reaction Conditions









Sample















1
2
3
4
5
6
7


















Temp. ° C.
95.0
95.0
95.0
95.0
95.0
95.0
95.0


Pressure, psig
399
398
399
399
299
299
299


C2 Part. Pressure, psi
90.0
90.0
89.9
90.0
73.3
73.5
52.3


H2/C2 Molar Ratio
0.60
0.40
0.90
0.83
0.600
0.614
0.584


C4/C2 Molar Ratio
0.000
0.000
0.000
0.000
0.000
0.000
0.000


C6/C2 Molar Ratio
0.033
0.034
0.031
0.032
0.033
0.020
0.060


IC5%
0.867
0.820
0.860
0.842
0.283
0.329
0.383


Cat Feed Rate ul/hr
4.8
3.5
5.4
5.4
3
3
3


Cocatalyst
2.5%
2.5%
2.5%
2.5%
2.5%
2.5%
2.5%



TEAL
TEAL
TEAL
TEAL
TEAL
TEAL
TEAL


Cocat. Feed Rate, cc/hr
210
183
231
210
128
130
134


Production Rate, lb/hr
28.3
28.3
24.6
26.5
25.0
24.9
24.9


Bed Weight, lbs
83.7
83.7
83.3
83.1
66.4
66.8
66.6


FBD (lb/ft{circumflex over ( )}3)
13.2
12.2
14.5
14.2
11.9
11.8
11.7


Bed Volume, ft{circumflex over ( )}3
6.3
6.9
5.7
5.9
5.6
5.7
5.7


Residence Time, hr
3.0
3.0
3.4
3.1
2.7
2.7
2.7


STY, lb/hr/ft{circumflex over ( )}3
4.5
4.1
4.3
4.5
4.5
4.4
4.4
















TABLE 1B







Resin Properties









Sample















1
2
3
4
5
6
7


















Melt Index, dg/min I2
21.3
7.4
65.6
48.5
19.73
17.80
22.93


Melt Index, dg/min I5
61.0
21.1
187.1
137.9
56.6
51.2
66.0


Flow Index, dg/min I21
548
182
1688
1238
517
461
604


Density, g/cc
0.9508
0.9474
0.9535
0.9525
0.9497
0.9537
0.9418


MFR (I21/I2)
25.7
24.6
25.7
25.5
26.2
25.9
26.3


MFR (I21/I5)
9.0
8.6
9.0
9.0
9.1
9.0
9.2


Residual Ti., ppm
1.74
1.42
2.14
2.18
2.36
2.34
3.28


Residual Al, ppm
57.0
48.5
59.1
62.0
74.0
110.0
71.0


Al/Ti molar
58.6
61.0
49.6
50.1
56.0
83.0
38.8


Bulk Density, lb/ft{circumflex over ( )}3
22.2
19.1
24.2
23.6
22.2
22.5
21.7


APS, inches
0.023
0.028
0.021
0.021
0.023
0.026
0.019


Fines, Wt % LT 120
2.40
1.06
2.20
2.93
2.04
1.80
4.52


Mesh










Linear Ethylene-Based Interpolymers


As discussed above the high molecular weight ethylene-based interpolymer and the low molecular weight ethylene-based interpolymer are each a linear ethylene-based interpolymer, and preferably a heterogeneously branched linear or a homogeneously branched linear ethylene-based interpolymer. The term “linear ethylene-based interpolymer,” as used herein, refers to an interpolymer that lacks long-chain branching, or lacks measurable amounts of long chain branching, as determined by techniques known in the art, such as NMR spectroscopy (for example 1C NMR as described by Randall, Rev. Macromal. Chem. Phys., C29 (2&3), pp. 285-293, incorporated herein by reference). Long-chain branched interpolymers are described in U.S. Pat. Nos. 5,272,236 and 5,278,272. As known in the art, the heterogeneously branched linear and homogeneously branched linear interpolymers have short chain branching due to the incorporation of comonomer into the growing polymer chain.


The terms “homogeneous” and “homogeneously-branched” are used in reference to an ethylene/α-olefin polymer (or interpolymer), in which the α-olefin comonomer is randomly distributed within a given polymer molecule, and substantially all of the polymer molecules have the same ethylene-to-comonomer ratio. These interpolymers are typically prepared using a metallocene catalyst system.


The homogeneously branched linear ethylene interpolymers are ethylene interpolymers, which lack long chain branching (or measurable amounts of long chain branching), but do have short chain branches, derived from the comonomer polymerized into the interpolymer, and in which the comonomer is homogeneously distributed, both within the same polymer chain, and between different polymer chains. Homogeneously branched linear ethylene interpolymers lack long chain branching, just as is the case for the linear low density polyethylene polymers or linear high density polyethylene polymers, made using uniform branching distribution polymerization processes as described, for example, by Elston in U.S. Pat. No. 3,645,992.


Commercial examples of homogeneously branched linear ethylene/α-olefin interpolymers include TAFMER™ polymers supplied by the Mitsui Chemical Company and EXACT™ and EXCEED™ polymers supplied by ExxonMobil Chemical Company.


In a preferred embodiment, the ethylene-based interpolymer is a heterogeneously branched linear ethylene interpolymer. Heterogeneously branched linear ethylene interpolymers include, but are not limited to, interpolymers of ethylene and one or more C3 to C8 α-olefins. Heterogeneously branched ethylene interpolymers can be prepared using Ziegler-Natta catalyst systems. Both the molecular weight distribution, and the short chain branching distribution, each arising from α-olefin (or comonomer) copolymerization, are relatively broad compared to homogeneously branched linear and homogeneously branched linear substantially linear ethylene interpolymers. Heterogeneously branched linear ethylene interpolymers can be made in a solution, slurry, or gas phase process using a Ziegler-Natta catalyst. For example, see U.S. Pat. No. 4,339,507, which is fully incorporated herein by reference.


Heterogeneously branched linear ethylene-based interpolymers differ from the homogeneously branched ethylene-based interpolymers, primarily in their comonomer branching distribution. For example, heterogeneously branched interpolymers have a branching distribution, in which the polymer molecules do not have the same ethylene-to-comonomer ratio. For example, heterogeneously branched LLDPE polymers have a distribution of branching, including a highly branched portion (similar to a very low density polyethylene), a medium branched portion (similar to a medium branched polyethylene) and an essentially linear portion (similar to linear homopolymer polyethylene).


As discussed above, heterogeneously branched ethylene-based interpolymers are typically prepared with a Ziegler/Natta catalyst system. These linear interpolymers lack long chain branching, or measurable amounts of long chain branching, as discussed above.


Heterogeneously branched ethylene-based interpolymers include, but are not limited to, linear medium density polyethylene (LMDPE), linear low density polyethylene (LLDPE), very low density polyethylene (VLDPE), and ultra low density polyethylene (ULDPE). Commercial polymers include DOWLEX™ polymers, ATTANE™ polymer, TUFLIN™ polymers, and FLEXOMER™ polymers (all from The DOW Chemical Company), and ESCORENE™ LLDPE polymers (from Exxon Mobil).


In preferred embodiment, the high molecular weight ethylene-based interpolymer is prepared using a Ziegler/Natta catalyst system, and the low molecular weight ethylene-based interpolymer is prepared using a Ziegler/Natta catalyst system.


In another embodiment, the high molecular weight ethylene-based interpolymer is a heterogeneously branched linear ethylene-based interpolymer, and the low molecular weight ethylene-based interpolymer is a heterogeneously branched linear ethylene-based interpolymer.


Polyethylene Blend


As discussed above, the blend of the invention comprises a high molecular weight ethylene-based interpolymer and a low molecular weight ethylene-based interpolymer. In a preferred embodiment, the blend is an in-situ blend. An in-situ blend is formed in a polymerization reactor (or reactor blend), as opposed to a post-reactor blend formed by mixing polymer components after the separate polymerization of each component.


The inventive blend has a single peak in an ATREF profile eluting above 30° C., and has a coefficient of viscosity average molecular weight (CMv) less than −0.0032, and preferably less than −0.0036, and more preferably less than −0.0040, in the log(calculated Mv) versus elution temperature, said CMv calculated in the range of elution temperatures from 70° C. to 90° C. Here Mv is the viscosity average molecular weight.


ATREF


General Overview


The inventive blend is characterized by ATREF (Analytical Temperature Rising Elution Fractionation), as described, for example, in Wild et al., Journal of Polymer Science, Poly. Phys. Ed., Vol. 20, p. 441 (1982); in U.S. Pat. No. 4,798,081 (Hazlitt et al.); or in U.S. Pat. No. 5,089,321 (Chum et al.), the disclosures of all of which are fully incorporated herein by reference. See also L. G. Hazlitt, J. Appl. Polym. Sci.: Appl. Poly. Symp., 45, 25-37 (1990), which is fully incorporated herein by reference.


In the technique of Analytical Temperature Rising Elution Fractionation (as described in U.S. Pat. No. 4,798,081), the polymer composition to be analyzed is dissolved in a suitable hot solvent (for example, 1,2,4-trichlorobenzene), and allowed to crystallized in a column containing an inert support (for example, stainless steel shot), by slowly reducing the temperature of the column. The column is equipped with both an (1) infra-red detector (for example, an IR-4 from Polymer ChAR, Valencia, Spain), or a refractive index, and (2) a differential viscometer (DV) detector. An ATREF-DV chromatogram curve is then generated by eluting the crystallized polymer sample from the column by slowly increasing the temperature of the column.


The ATREF curve is also frequently called the short chain branching distribution (SCBD), since it indicates how the comonomer (for example, hexene) is distributed throughout the sample, in that as elution temperature decreases, comonomer content increases. The IR detector provides concentration of polymer as a function of temperature, which can be used to generate the short chain branching distribution. The differential viscometer detector provides an estimate of the viscosity average molecular weight at each elution temperature (see U.S. Pat. No. 4,798,081). The generated curves that show data obtained from both the IR detector and the differential viscometer detector are known as, collectively, an ATREF-DV overlay profile.


The inventive blends show a characteristic decrease in the measured viscosity average molecular weight (Mv) as the column temperature increases. This decrease in the Mv is observed especially in the region from 70° C. to 90° C. In this region (70° C.-90° C.), a regression slope can be calculated from the log(Mv) versus elution temperature, using a linear regression technique, such as available in the EXCEL program LINEST (MicroSoft Corp., Redmond, Wash.). The regression slope is also denoted as the coefficient of the viscosity average molecular weight (CMv).


A more detailed description of the Analytical Temperature Rising Elution Fractionation-Differential Viscometry (ATREF-DV) analysis is described below.


Determination of the Coefficient of Viscosity Average Molecular Weight (CMv) Using ATREF-DV


Fractionation by Analytical Temperature Rising Elution Fractionation-Differential Viscometry, ATREF-DV, was performed on the polymer samples, using the methods and apparatus described by Wild1 and Hazlitt2,3. The column was constructed from ⅛″×18″ thin-wall stainless-steel tubing, and packed with 0.023″×0.023″ stainless-steel shot from Pellets Inc. (Tonawanda, New York). The column had a 1.5 ml interstitial volume. 1 L. Wild, T. R. Ryle, D. C. Knobeloch, and I. R. Peat, Journal of Polymer Science: Polymer Physics Edition, Vol. 20, 441-455 (1982).2 L. Hazlitt and D. Moldovan, U.S. Pat. No. 4,798,081, 1989.3 L. Hazlitt, Journal of Applied Polymer Science: Applied Polymer Symposia, 45, 25-37 (1990).


A controlled GC (Gas Chromatography) oven was used to affect the temperature profiles. Two additional ovens provided high temperature thermal control, respectively, for the sample loading chamber, and a value section, which contained various valves for directing solvent flow. These later two ovens were maintained at 130° C.


As discussed above, the polymer sample was dissolved in a suitable solvent, such as 1,2,4-trichlorobenzene (containing 180 ppm BHT as an antioxidant) to form a polymer solution. The initial polymer concentration was between 50 mg and 200 mg in 50 ml (at room temperature) of the 1,2,4-trichlorobenzene (TCB), and this concentration was adjusted to accommodate the sharpness of the eluting peaks, so that it would not exceed the maximum response for the concentration and viscosity detection in the data collection hardware. Such adjustments can be made by one skilled in the art.


The polymer solution was deposited on the stainless steal column, at a column temperature of 130° C. Once deposited on the column, the temperature of the column was decreased at a maintained rate of −0.1° C./min, to a final column temperature of about 20° C. Next, the elution temperature was increased at a rate of 1.0° C./min, from 20° C. to 122° C. The solvent elution also began at this time, and the solvent (1,2,4-trichlorobenzene containing 180 ppm BHT as an antioxidant) flow rate was 1.0 ml/min. The elution was directed, via heated transfer lines, to, first, an IR-44 infrared detector, second, PD2040 low angle laser light scattering (LALLS) detector5, and finally a Model H502C differential viscometer6. Each detector was maintained at a temperature of 140° C. A reservoir for solvent waste was provided after the sequence of detectors. Temperature control, valve sequencing and data collection were achieved using LabView7 software8 on a personal computer. 4 Sold by PolymerChar of Valencia, Spain.5 Sold by Precision Detectors of Bellingham Mass.6 Sold by Viscotek of Houston, Tex.7 Trademark of National Instruments of Austin, Tex.8 Written under contract with Quantum Automation of Houston, Tex.


The data collected for each copolymer, during each elution of the ATREF-DV apparatus, consisted of the column elution temperature [RTD, Ti(° C.)], the mass or concentration response [infrared detector, IRi(mv)], the differential viscosity response [differential viscometer, DPi(mv)], the Inlet Pressure [differential viscometer, IPi(mv)], and the light scattering response [LALLS detector, LSi(mv)]. These are collected at five second intervals. The detector offsets or lag times are corrected in the data processing step. The various detectors are calibrated by using polymers of known weight average molecular weight and intrinsic viscosity9. The baseline subtracted data is used in the following equations, where the subscripted i represents an arbitrary data point. 9 A. Degroot et al, Waters International GPC Conference (1998).


Equation 1 shows the relationship between the intrinsic viscosity, [η]0, and the viscosity average molecular weight, Mv, for the whole polymer. The values of K and a are 6.3*10−4 and 0.7, respectively.










M
v

=


{


1
K

·


[
η
]

0


}


1
/
a






(

Equation





1

)







Equation 2 describes how the differential viscosity, ηi, and the inlet pressure, Inlet, Pi, is used to estimate [η]0,i for an arbitrary data point using the concentration, ci.











[
η
]


0
,
i


=



4
·

η
i




Inlet





_






P
i


-

2
·

η
i




/

c
i






(

Equation





2

)







Equation 3 describes how to calculate the viscosity average molecular weight, Mv,i.










M

v
,
i


=


[


1
K

·



4
·

η
i




IP
i

-

2
·

η
i





c
i



]


1
/
a






(

Equation





3

)







Equations 4 and 5 describe how to use the signals from the viscometer, DPi and IPi to estimate the differential viscosity, ηi, and the inlet pressure, Inlet_Pi.

ηi=kDP·DPi  (Equation 4)
InletPi=kIP·IP  (Equation 5)


Equation 6 describes how to calculate the concentration, ci, for an arbitrary point from the IR response, IRi.

ci=kIR·IRi  (Equation 6)


Equation 7 shows the normalization step needed to calculate the overall moments, Mv and Mw.










C
total

=



i




c
i

·

w
i







(

Equation





7

)







Equation 8 shows how to calculate the weight average molecular weight for an arbitrary point.










M

w
,
i


=



k
LS

·

LS
i



c
i






(

Equation





8

)







Equations 9 and 10 are used to estimate the values of the various detector constants, kDP, kIP, kIR and kLS, using at least two different polymers, for which the intrinsic viscosity and the weight average molecular weight are known, and adjusting the detector constants, until the proper moments are obtained.










M
v

=


[




i




c
i

·

M

v
,
i

a




C
total


]


1
/
a






(

Equation





9

)







M
w

=




i




c
i

·

M

w
,
i





C
total






(

Equation





10

)







Alternatively, the viscometer can be calibrated using methods described by the manufacturer, and the remaining coefficients, kIR, and kLS, can be obtained as described above. For the purposes of the current invention, only the viscosity average molecular weight, Mv,i, is required.


As discussed above, the viscosity average molecular weights, Mv,i, and the elution temperatures, Ti, are used to calculate the coefficient of viscosity average molecular weight, CMv, using simple linear regression. This coefficient is the slope for the regression line (log(Mv) vs. elution temperature) using the points between 70° C. and 90° C. in the ATREF-DV data. The values of the logarithm of the viscosity average molecular weights, Log Mv,i, are treated as the y values, and the elution temperatures, Ti, are treated as the x values. As discussed above, the regression slope can be obtained using commercially available routines, such as the function LINEST in EXCEL10. 10 Sold by Microsoft Corp.


Polyethylene Composition


In one embodiment, the composition has a density greater than, or equal to, 0.930 g/cc, preferably greater than, or equal to, 0.932 g/cc, and more preferably greater than, or equal to, 0.935 g/cc and most preferably greater than or equal to 0.9375 g/cc. In another embodiment, composition has a density less than, or equal to, 0.945 g/cc, preferably less than, or equal to, 0.942 g/cc. In another embodiment, the composition has a density from 0.930 to 0.945 g/cc, and preferably from 0.932 to 0.943 g/cc, and more preferably from 0.935 to 0.942 g/cc, and most preferably from 0.9375-0.942 g/cc.


In a preferred embodiment, composition has a high load melt index, I21, (190° C., 21.6 kg weight, ASTM 1238-03) greater than, or equal to, 5, preferably greater than, or equal to, 6, and more preferably greater than, or equal to, 7 (units of grams per 10 minutes). In another embodiment, composition has a high load melt index, I21 less than, or equal to, 18, preferably less than, or equal to, 16, and more preferably greater than, or equal to, 14. In yet another embodiment, the I21 ranges from 5 to 18 grams per 10 minutes, and preferably in the range from 7 to 15 grams per 10 minutes, and more preferably in the range from 7.5 to 12 grams per 10 minutes. A composition with a high load melt index less than 5 will be more difficult to extrude.


In another embodiment, the high molecular weight ethylene-based interpolymer is present in an amount less than, or equal to 60 weight percent, preferably less than, or equal to 58 weight percent, and more preferably less than, or equal to 55 weight percent, based on the sum weight of the high molecular weight ethylene-based interpolymer and the low molecular weight ethylene-based interpolymer. In another embodiment, the low molecular weight ethylene-based interpolymer is present in an amount greater than, or equal to 40 weight percent, preferably greater than, or equal to 42 weight percent, and more preferably greater than, or equal to 45 weight percent, based on the sum weight of the high molecular weight ethylene-based interpolymer and the low molecular weight ethylene-based interpolymer. In another embodiment, the weight ratio of the high molecular weight component to the low molecular weight component (HMW/LMW) is from 60/40 to 45/55, and more preferably from 55/45 to 45/55.


The composition may comprise a combination of two or more embodiments as described herein.


Catalysts


Typical transition metal catalyst systems, which can be used to prepare the inventive blend, are Ziegler-Natta catalyst systems, such as magnesium/titanium based catalyst systems, which can be exemplified by the catalyst system described in U.S. Pat. No. 4,302,565, incorporated herein by reference. See also WO 2006/023057, and WO 2005/012371, each incorporated herein by reference.


In some embodiments, preferred catalysts used in the process to make the blends of the present invention are of the magnesium/titanium type. In particular, for gas phase polymerizations, the catalyst is made from a precursor comprising magnesium and titanium chlorides in an electron donor solvent. This solution is often either deposited on a porous catalyst support, or a filler is added, which, on subsequent spray drying, provides additional mechanical strength to the particles. The solid particles from either support methods are often slurried in a diluent, producing a high viscosity mixture, which is then used as catalyst precursor. Exemplary catalyst types are described in U.S. Pat. No. 6,187,866 and U.S. Pat. No. 5,290,745, the entire contents of both are herein incorporated by reference. Precipitated/crystallized catalyst systems, such as those described in U.S. Pat. No. 6,511,935 and U.S. Pat. No. 6,248,831, the entire contents of both are herein incorporated by reference, may also be used.


In one embodiment, the catalyst precursor has the formula MgdTi(OR)eXf(ED)g, wherein R is an aliphatic or aromatic hydrocarbon radical having 1 to 14 carbon atoms or COR′, wherein R′ is a aliphatic or aromatic hydrocarbon radical having 1 to 14 carbon atoms; each OR group is the same or different; X is independently chlorine, bromine or iodine; ED is an electron donor; d is 0.5 to 56; e is 0, 1, or 2; f is 2 to 116; and g is >2 and up to 1.5*d+3. Such a precursor is prepared from a titanium compound, a magnesium compound, and an electron donor.


The electron donor is an organic Lewis base, liquid at temperatures in the range of about 0° C. to about 200° C., and in which the magnesium and titanium compounds are soluble. The electron donor compounds are sometimes also referred to as Lewis bases. The electron donor can be an alkyl ester of an aliphatic or aromatic carboxylic acid, an aliphatic ketone, an aliphatic amine, an aliphatic alcohol, an alkyl or cycloalkyl ether, or mixtures thereof, and each electron donor having 2 to 20 carbon atoms. Among these electron donors, the preferred are alkyl and cycloalkyl ethers having 2 to 20 carbon atoms; dialkyl, diaryl, and alkylaryl ketones having 3 to 20 carbon atoms; and alkyl, alkoxy, and alkylalkoxy esters of alkyl and aryl carboxylic acids having 2 to 20 carbon atoms. The most preferred electron donor is tetrahydrofuran. Other examples of suitable electron donors are methyl formate, ethyl acetate, butyl acetate, ethyl ether, dioxane, di-n-propyl ether, dibutyl ether, ethanol, 1-butanol, ethyl formate, methyl acetate, ethyl anisate, ethylene carbonate, tetrahydropyran, and ethyl propionate.


While a large excess of electron donor may be used initially to provide the reaction product of titanium compound and electron donor, the final catalyst precursor contains about 1 to about 20 moles of electron donor per mole of titanium compound, and preferably about 1 to about 10 moles of electron donor per mole of titanium compound.


Since the catalyst will act as a template for the growth of the polymer, it is essential that the catalyst precursor be converted into a solid. It is also essential that the resultant solid has the appropriate particle size and shape to produce polymer particles with relatively narrow size distribution, low amounts of fines and good fluidization characteristics. Although this solution of Lewis Base, magnesium and titanium compounds may be impregnated into a porous support, and dried to form a solid catalyst, it is preferred that the solution be converted into a solid catalyst via spray drying. Each of these methods thus forms a “supported catalyst precursor.” The spray dried catalyst product is then, preferentially placed into mineral oil slurry. The viscosity of the hydrocarbon slurry diluent is sufficiently low, so that the slurry can be conveniently pumped through the pre-activation apparatus, and eventually into the polymerization reactor. The catalyst is fed using a slurry catalyst feeder. A progressive cavity pump, such as a Moyno pump, is typically used in commercial reaction systems, while a dual piston syringe pump is typically used in pilot scale reaction systems, where the catalyst flows are less than, or equal to, 10 cm3/hour (2.78×10-9 m3/s) of slurry.


A cocatalyst, or activator, is also fed to the reactor to effect the polymerization. Complete activation by additional cocatalyst is required to achieve full activity. The complete activation normally occurs in the polymerization reactor, although the techniques taught in EP 1,200,483, incorporated herein by reference, may also be used.


The cocatalysts, which are reducing agents, are typically comprised of aluminum compounds, but compounds of lithium, sodium and potassium, alkaline earth metals, as well as compounds of other earth metals, other than aluminum are possible. The compounds are usually hydrides, organometal or halide compounds. Butyl lithium and dibutyl magnesium are examples of useful compounds.


An activator compound, which is generally used with any of the titanium based catalyst precursors, can have the formula AlRaXbHc, wherein each X is independently chlorine, bromine, iodine, or OR′; each R and R′ is independently a saturated aliphatic hydrocarbon radical having 1 to 14 carbon atoms; b is 0 to 1.5; c is 0 or 1; and a+b+c=3. Preferred activators include alkylaluminum mono- and dichlorides, wherein each alkyl radical has 1 to 6 carbon atoms, and the trialkylaluminums. Examples are diethylaluminum chloride and tri-n-hexylaluminum. About 0.10 moles to about 10 moles, and preferably about 0.15 moles to about 2.5 moles, of activator are used per mole of electron donor. The molar ratio of activator to titanium is in the range of about 1:1 to about 10:1, and is preferably in the range of about 2:1 to about 5:1.


The hydrocarbyl aluminum cocatalyst can be represented by the formula R3Al or R2AlX, wherein each R is independently alkyl, cycloalkyl, aryl, or hydrogen; at least one R is hydrocarbyl; and two or three R radicals can be joined to form a heterocyclic structure. Each R, which is a hydrocarbyl radical, can have 1 to 20 carbon atoms, and preferably has 1 to 10 carbon atoms. X is a halogen, preferably chlorine, bromine, or iodine. Examples of hydrocarbyl aluminum compounds are as follows: triisobutylaluminum, tri-n-hexylaluminum, di-isobutyl-aluminum hydride, dihexylaluminum hydride, di-isobutylhexylaluminum, isobutyl dihexylaluminum, trimethylaluminum, triethylaluminum, tripropylaluminum, triisopropylaluminum, tri-n-butylaluminum, trioctylaluminum, tridecylaluminum, tridodecylaluminum, tribenzylaluminum, triphenylaluminum, trinaphthylaluminum, tritolylaluminum, dibutylaluminum chloride, diethylaluminum chloride, and ethylaluminum sesquichloride. The cocatalyst compounds can also serve as activators and modifiers.


Activators can be added to the precursor either before and/or during polymerization. In one procedure, the precursor is fully activated before polymerization. In another procedure, the precursor is partially activated before polymerization, and activation is completed in the reactor. Where a modifier is used, instead of an activator, the modifiers are usually dissolved in an organic solvent, such as isopentane. Where a support is used, the modifier is typically impregnated into the support, following impregnation of the titanium compound or complex, after which the supported catalyst precursor is dried. Otherwise, the modifier solution is added by itself directly to the reactor. Modifiers are similar in chemical structure and function to the activators, as are cocatalysts. For variations, see for example, U.S. Pat. No. 5,106,926, incorporated herein by reference in its entirety. The cocatalyst is preferably added separately neat, or as a solution in an inert solvent, such as isopentane, to the polymerization reactor at the same time as the flow of ethylene is initiated.


In those embodiments that use a support, the precursor is supported on an inorganic oxide support, such as silica, aluminum phosphate, alumina, silica/alumina mixtures, silica that has been modified with an organoaluminum compound, such as triethyl aluminum, and silica modified with diethyl zinc. In some embodiments silica is a preferred support. A typical support is a solid, particulate, porous material essentially inert to the polymerization. It is used as a dry powder having an average particle size of about 10 μm to about 250μ, and preferably about 30 μm to about 100 μm; a surface area of at least 200 m2/g and preferably at least about 250 m2/g; and a pore size of at least about 100×10-10 m and preferably at least about 200×10-10 m. Generally, the amount of support used, is that which will provide about 0.1 millimole to about 1.0 millimole of titanium per gram of support, and preferably about 0.4 millimole to about 0.9 millimole of titanium per gram of support. Impregnation of the above mentioned catalyst precursor into a silica support can be accomplished by mixing the precursor and silica gel in the electron donor solvent, or other solvent, followed by solvent removal under reduced pressure. When a support is not desired, the catalyst precursor can be used in liquid form.


Polymerization


The novel composition can be made by a variety of methods. For example, it may be made by blending or mixing the high molecular weight interpolymer and the low molecular weight interpolymer, or by melt-blending the individually melted components. Alternatively, it may be made in situ, in one or more polymerization reactors, including, but not limited to, a dual reactor configuration.


In a preferred dual reactor configuration of the process of the present invention, the catalyst precursor and the cocatalyst are introduced in the first reactor, and the polymerizing mixture is transferred to the second reactor for further polymerization. Insofar as the catalyst system is concerned, only cocatalyst, if desired, is added to the second reactor from an outside source. Optionally the catalyst precursor may be partially activated prior to the addition to the reactor (preferably the first reactor), followed by further “in reactor activation” by the cocatalyst.


In the preferred dual reactor configuration, a relatively high molecular weight (low melt flow index) copolymer is prepared in the first reactor. Alternatively, the low molecular weight copolymer can be prepared in the first reactor, and the high molecular weight copolymer can be prepared in the second reactor. For purposes of the present disclosure, the reactor, in which the conditions are conducive to making a high molecular weight polymer, is known as the “high molecular weight reactor”. Alternatively, the reactor, in which the conditions are conducive to making a low molecular weight polymer, is known as the “low molecular weight reactor.” Irrespective of which component is made first, the mixture of polymer and an active catalyst is preferably transferred from the first reactor to the second reactor, via an interconnecting device, using nitrogen, or second reactor recycle gas, as a transfer medium.


The polymerization in each reactor is preferably conducted in the gas phase using a continuous fluidized bed process. In a typical fluidized bed reactor, the bed is usually made up of the same granular resin that is to be produced in the reactor. Thus, during the course of the polymerization, the bed comprises formed polymer particles, growing polymer particles, catalyst particles fluidized by polymerization, and modifying gaseous components, introduced at a flow rate or velocity sufficient to cause the particles to separate and act as a fluid. The fluidizing gas is made up of the initial feed, make-up feed, and cycle (recycle) gas, that is, comonomers, and, if desired, modifiers and/or an inert carrier gas.


A typical fluid bed system includes a reaction vessel, a bed, a gas distribution plate, inlet and outlet piping, a compressor, cycle gas cooler, and a product discharge system. In the vessel, above the bed, there is a velocity reduction zone, and, in the bed, a reaction zone. Both are above the gas distribution plate. A typical fluidized bed reactor is further described in U.S. Pat. No. 4,482,687, the entire contents of which are herein incorporated by reference.


The gaseous feed streams of ethylene, other gaseous alpha-olefins, and hydrogen, when used, are preferably fed to the reactor recycle line, as well as liquid or gaseous alpha-olefins and the cocatalyst solution. Optionally, the liquid cocatalyst can be fed directly to the fluidized bed. The partially activated catalyst precursor is preferably injected into the fluidized bed as a mineral oil slurry. Activation is generally completed in the reactors by the cocatalyst. The product composition can be varied by changing the molar ratios of the monomers introduced into the fluidized bed. The product is continuously discharged in granular or particulate form from the reactor, as the bed level builds up with polymerization. The production rate is controlled by adjusting the catalyst feed rate and/or the ethylene partial pressures in both reactors.


A preferred mode is to take batch quantities of product from the first reactor, and transfer these to the second reactor using the differential pressure generated by the recycle gas compression system. A system similar to that described in U.S. Pat. No. 4,621,952, the entire contents of which are herein incorporated by reference, is particularly useful.


The pressure is about the same in both the first and second reactors. Depending on the specific method used to transfer the mixture of polymer and contained catalyst from the first reactor to the second reactor, the second reactor pressure may be either higher than, or somewhat lower than, that of the first. If the second reactor pressure is lower, this pressure differential can be used to facilitate transfer of the polymer catalyst mixture from Reactor 1 to Reactor 2. If the second reactor pressure is higher, the differential pressure across the cycle gas compressor may be used as the motive force to move polymer. The pressure, that is, the total pressure in either reactor, can be in the range of about 200 to about 500 psig (pounds per square inch gauge), and is preferably in the range of about 270 to about 450 psig (1.38, 3.45, 1.86 and 3.10 MPa, respectively). The ethylene partial pressure in the first reactor can be in the range of about 10 to about 150 psig, and is preferably in the range of about 20 to about 80 psig, and more preferably is in the range of about 25 to about 60 psig, (68.9, 1034, 138, 552, 172 and 414 MPa, respectively). The ethylene partial pressure in the second reactor is set according to the amount of copolymer to be produced in this reactor, to achieve the appropriate split. It is noted that increasing the ethylene partial pressure in the first reactor leads to an increase in ethylene partial pressure in the second reactor. The balance of the total pressure is provided by alpha-olefin other than ethylene and an inert gas such as nitrogen. Other inert hydrocarbons, such as an induced condensing agent, for example, isopentane or hexane, also contribute to the overall pressure in the reactor, according to their vapor pressure, under the temperature and pressure experienced in the reactor.


The hydrogen:ethylene mole ratio can be adjusted to control average molecular weights. The alpha-olefins (other than ethylene) can be present in a total amount of up to 15 percent by weight of the copolymer, and, if used, are preferably included in the copolymer in a total amount from about 0.5 to about 10 percent by weight, or more preferably from about 0.8 to about 4 percent by weight, based on the weight of the copolymer.


The residence time of the mixture of reactants including gaseous and liquid reactants, catalyst, and resin, in each fluidized bed can be in the range from about 1 to about 12 hours, and is preferably in the range from about 1.5 to about 5 hours. The reactors can be run in the condensing mode, if desired. The condensing mode is described in U.S. Pat. No. 4,543,399, U.S. Pat. No. 4,588,790 and U.S. Pat. No. 5,352,749, the entire content of each is herein incorporated by reference.


While the polyethylene blends of subject invention are preferably produced in the gas phase by various low pressure processes, the blend can also be produced in the liquid phase in solutions or slurries by conventional techniques, again at low pressures. Low pressure processes are typically run at pressures below 1000 psi, whereas high pressure processes are typically run at pressures above 15,000 psi (6.89 and 103 MPa, respectively).


As discussed above, in a dual reactor system, the high molecular weight component or the low molecular weight component can be prepared in the first reactor or second reactor. Dual reactor systems include, but are not limited to, two gas phase fluidized bed reactors in series, two stirred tank reactors in series, two loop reactors in series, two solution spheres or loops in series, or a suitable combination of two reactors. For the reaction of interest, appropriate comonomer amounts, ethylene partial pressures, and temperatures will be adjusted to produce the desired composition. Such adjustments can be made by those skilled in the art.


High Molecular Weight Reactor Operation Conditions


In an embodiment suitable for pipes, operating temperature can range from about 70° C. to about 110° C. The mole ratio of alpha-olefin to ethylene in this reactor can be in the range of from about 0.03:1 to about 0.105:1, and is preferably in the range of from about 0.04:1 to about 0.1:1 and most preferably from about 0.050:1 to about 0.095:1. The mole ratio of hydrogen (if used) to ethylene in this reactor can be in the range of from about 0.01:1 to about 0.09:1, preferably of from about 0.02 to about 0.05:1.


In an embodiment suitable for blown films, the high molecular weight reactor operating temperature is generally in the range from about 70° C. to about 110° C. The operating temperature is preferably varied with the desired density to avoid product stickiness in the reactor. The mole ratio of alpha-olefin to ethylene can be in the range from about 0.03 to about 0.105:1, preferably in the range from about 0.04:1 to about 0.1:1. The mole ratio of hydrogen to ethylene can be in the range from about 0.01:1 to about 0.09:1, and is preferably in the range from about 0.02:1 to about 0.05:1.


In an embodiment suitable for blow molding, the high molecular weight reactor operating temperature is generally in the range from about 70° C. to about 110° C. The operating temperature is preferably varied with the desired density to avoid product stickiness in the reactor. The mole ratio of alpha-olefin to ethylene can be in the range from about 0.03:1 to about 0.105:1, preferably in the range from about 0.04:1 to about 0.1:1. The mole ratio of hydrogen to ethylene can be in the range from about 0.01:1 to about 1:1, and is preferably in the range from about 0.02:1 to about 0.05:1.


Low Molecular Weight Reactor Operation Conditions


In an embodiment suitable for pipes, blown films and blow molding, the operating temperature is generally in the range from about 70° C. to about 110° C. The mole ratio of alpha-olefin to ethylene can be in the range from about 0.01 to about 0.065:1, preferably in the range from about 0.015:1 to about 0.055:1. The mole ratio of hydrogen to ethylene can be in the range from about 0.1:1 to about 1:1, and is preferably in the range from about 0.2:1 to about 0.95:1.


Additives


The inventive compositions may contain one or more additional components or additives. Suitable additional components include, for example, other polymers, fillers or additives, with the proviso that these additional components do not adversely interfere with the desired advantageous properties of the compositions of the invention. Rather, the additional components are selected such as to support the advantageous properties of an inventive composition and/or to support, or enhance, the composition's particular suitability for a desired application. “Other polymers,” comprised in the composition of the invention, means polymers which do not qualify as a HMW interpolymer or a LMW interpolymer, as defined herein. Advantageously, such polymers are compatible with the inventive composition.


Preferred additional components are non polymeric. Additives include processing aids, acid neutralizers, UV stabilizers, antioxidants, process stabilizers, metal de-activators, additives to improve oxidative or chlorine resistance, pigments or colorants.


Effective additive packages are needed to protect the excellent mechanical properties during the life time of the fabricated parts, where the parts are exposed to UV or chlorine environment. A mixture of hindered amines, such as Cyasorb UV 3529, Chemisorb™ 944, 2020, 622, Hostavin™ N30, and the like, and UV absorbers, such as Cyasorb™ 531, Tinuvin™ 327, 328, 329, Cyasorb™ THT, and the like, can be used to stabilizer the polymer against the degradation by UV light. The preferred UV additive composition is the mixture of Cyasorb™ UV 531 and Cyasorb™ UV-3529. For domestic pipe applications, where chlorine resistance is needed, a synergetic antioxidant system comprising two or more hindered phenols is used. The first class of hindered phenols comprises the hindered phenols that exhibit excellent antioxidant reactivity (oxidation by oxygen or chlorine), such as IRGANOX™ I-1010, IRGANOX™ I-1076, or/and Hostanox™ O3. The second class of hindered phenol comprises the hindered phenols that have a good water extraction resistance, such as IROGANOX I-1330. In addition metal deactivators, like IROGANOX I-1024 or Naugard XL1, are employed in pipe installations where metal fittings maybe used.


In a preferred embodiment, the total range for UV stabilizers is from 100 to 8000 ppm, with a preferred range from 1000 ppm to 4000 ppm. In another embodiment, the total range of antioxidant/chlorine resistance additives is from 100 to 9000 ppm, with a preferred range from 1000 ppm to 6000 ppm. The preferred range for metal deactivators is from 300 to 2000 ppm.


Stabilizers to protect against degradation or consumption of additives during conversion from granular form to pellets, and in the extrusion of the pipe resin include phosphites. These act to prevent degradation of the phenolic type stabilizers so they are not consumed prior to the pipe being put into long term usage. Stabilizers include TNPP, Irgafos 168, Doverphos 9228, PEPQ, and others. A preferred phosphite is Irgafos 168 or Doverphos 9228. Preferred ranges are from 250 to 2000 ppm levels, more preferred levels are from 750 to 1800 ppm.


In one embodiment, an inventive composition contains one or more additives are selected from hindered amines, hindered phenols, metal deactivators, UV absorbers, phosphites, acid neutralizers, processing aids, and combinations thereof. In a further embodiment, the one or more additives are selected from Cyasorb 3529, Irganox 1010, Irganox 1076, Irganox 1330, Irganox MD1024, Irgafos 168, calcium stearate, Dynamar FX 5911, and combinations thereof. In yet another embodiment, the one or more additives are selected from Cyasorb 3529, Irganox 1010, Irganox 1076, Irganox 1330, Irganox MD1024, Doverphos 9228, calcium stearate, Dynamar FX 5911, and combination thereof. In yet another embodiment, the one or more additives are selected from the group consisting of UV N30, Irganox 1330, Doverphos 9228, Irganox MD1024, HO3, calcium stearate, Dynamar FX 5911, and combinations thereof.


Fabricated Articles


The compositions of the present invention can be used to manufacture a shaped article, or one or more components of a shaped article. Such articles may be single-layer or a multi-layer articles, which are typically obtained by suitable known conversion techniques, applying heat, pressure, or a combination thereof, to obtain the desired article. Suitable conversion techniques include, for example, blown film, cast film, co-extrusion, lamination, blow-molding, co-extrusion blow-molding, injection molding, injection stretch blow molding, compression molding, extrusion, pultrusion, calendering and thermoforming. Shaped articles provided by the invention include, for example, films, pipes, drip tapes and tubings, geomembranes, sheets, fibers, laminates, profiles and moldings. Inventive films include, but are not limited to, blown films, cast films and co-extruded films.


Film and film structures can be made using the novel compositions as described herein using conventional blown film fabrication techniques or other, biaxial, orientation processes, such as tenter frames or double bubble processes. Conventional hot blown film processes are described, for example, in The Encyclopedia of Chemical Technology, Kirk-Othmer, Third Edition, John Wiley & Sons, New York, 1981, Vol. 16, pp. 416-417 and Vol. 18, pp. 191-192; incorporated herein by reference. Biaxial orientation film manufacturing process, such as described in a “double bubble” process, as in U.S. Pat. No. 3,456,044 (Pahlke), and the processes described in U.S. Pat. No. 4,352,849 (Mueller), U.S. Pat. No. 4,597,920 (Golike), U.S. Pat. No. 4,820,557 (Warren), U.S. Pat. No. 4,837,084 (Warren), U.S. Pat. No. 4,865,902 (Golike et al.), U.S. Pat. No. 4,927,708 (Herran et al.), U.S. Pat. No. 4,952,451 (Mueller), U.S. Pat. No. 4,963,419 (Lustig et al.), and U.S. Pat. No. 5,059,481 (Lustig et al.), can also be used to make film structures from the novel compositions described herein. The disclosure of each is incorporated herein by reference. The film structures can also be made as described in a tenter-frame technique, such as that used for oriented polypropylene. Polymer compositions may be rheology modified to improve bubble stability.


Other multi-layer film manufacturing techniques for food packaging applications are described in Packaging Foods With Plastics, by Wilmer A. Jenkins and James P. Harrington (1991), pp. 19-27, and in “Coextrusion Basics” by Thomas I. Butler, Film Extrusion Manual: Process, Materials, Properties pp. 31-80 (published by the TAPPI Press (1992)); the disclosure of each is incorporated herein by reference.


The films may be monolayer or multilayer films. The film made from an inventive composition can also be coextruded with the other layer(s), or the film can be laminated onto another layer(s) in a secondary operation, such as that described in Packaging Foods With Plastics, by Wilmer A. Jenkins and James P. Harrington (1991) or that described in “Coextrusion For Barrier Packaging” by W. J. Schrenk and C. R. Finch, Society of Plastics Engineers RETEC Proceedings, Jun. 15-17, 1981, pp. 211-229; the disclosure of each is incorporated herein by reference. If a monolayer film is produced via tubular film (i.e., blown film techniques, preferably on grooved barrel extruders) or flat die (i.e., cast film), as described by K. R. Osborn and W. A. Jenkins in “Plastic Films, Technology and Packaging Applications” (Technomic Publishing Co., Inc., 1992), the disclosure of which is incorporated herein by reference, then the film must go through an additional post-extrusion step of adhesive or extrusion lamination to other packaging material layers to form a multilayer structure. If the film is a coextrusion of two or more layers (also described by Osborn and Jenkins), the film may still be laminated to additional layers of packaging materials, depending on the other physical requirements of the final film. “Laminations vs. Coextrusion” by D. Dumbleton (Converting Magazine (September 1992), also discusses lamination versus coextrusion. Monolayer and coextruded films can also go through other post extrusion techniques, such as radiation induced cross-linking of the polymer and a biaxial orientation process.


The films and film layers of this invention are especially useful in vertical form-fill-seal (VFFS) applications. Patents describing improvements for VFFS applications, especially polymer improvements, include U.S. Pat. No. 5,228,531; U.S. Pat. No. 5,360,648; U.S. Pat. No. 5,364,486; U.S. Pat. No. 5,721,025; U.S. Pat. No. 5,879,768; U.S. Pat. No. 5,942,579; U.S. Pat. No. 6,117,465; each incorporated herein by reference.


Generally for a multilayer film structure, the novel compositions described herein comprise at least one layer of the total multilayer film structure. Other layers of the multilayer structure include, but are not limited to, barrier layers, and/or tie layers, and/or structural layers. Various materials can be used for these layers, with some of them being used as more than one layer in the same film structure. Some of these materials include: foil, nylon, ethylene/vinyl alcohol (EVOH) copolymers, polyvinylidene chloride (PVDC), polyethylene terephthalate (PET), oriented polypropylene (OPP), ethylene/vinyl acetate (EVA) copolymers, ethylene/acrylic acid (EAA) copolymers, ethylene/methacrylic acid (EMAA) copolymers, LLDPE (linear low density polyethylene), HDPE (high density polyethylene), LDPE (low density polyethylene), nylon, graft adhesive polymers (e.g., maleic anhydride grafted polyethylene), and paper. Generally, the multilayer film structures comprise from 2 to 7 layers.


The invention also provides a film comprising at least one component formed from an inventive composition. The film may be a multi-layered film or a single layered film. Preferably, the film has a thickness from 2 mils to 50 mils, preferably from 3 mils to 30 mils, and more preferably from 4 mils to 20 mils. In yet a further embodiment, the composition can also be made into a sheet, via either the blown or cast film process. The sheet can be from 2 to 200 mils or 10 to 150 mils or 20 to 100 mils thick.


In another embodiment, the film has an Elmendorf Tear Strength, in the machine direction (MD), greater than, or equal to, 100 g/mil, preferably greater than, or equal to, 120 g/mil, and more preferably greater than, or equal to 140 g/mil.


In another embodiment, the film has an Elmendorf Tear Strength, in the traverse direction (TD), greater than, or equal to, 220 g/mil, preferably greater than, or equal to, 240 g/mil, and more preferably greater than, or equal to 260 g/mil.


In another embodiment, the film has a Normalized Dart Impact (B scale) greater than, or equal to, 60 g, preferably greater than, or equal to, 80 g, and more preferably greater than, or equal to 100 g. The invention also provides an article comprising an inventive film or sheet. Preferably, the article is a shipping sack, a geomembrane, or a drip tape.


DEFINITIONS

Any numerical range recited herein, includes all values from the lower value and the upper value, in increments of one unit, provided that there is a separation of at least two units between any lower value and any higher value. As an example, if it is stated that a compositional, physical or other property, such as, for example, molecular weight, melt index, is from 100 to 1,000, it is intended that all individual values, such as 100, 101, 102, etc., and sub ranges, such as 100 to 144, 155 to 170, 197 to 200, etc., are expressly enumerated in this specification. For ranges containing values which are less than one, or containing fractional numbers greater than one (e.g., 1.1, 1.5, etc.), one unit is considered to be 0.0001, 0.001, 0.01 or 0.1, as appropriate. For ranges containing single digit numbers less than ten (e.g., 1 to 5), one unit is typically considered to be 0.1. These are only examples of what is specifically intended, and all possible combinations of numerical values between the lowest value and the highest value enumerated, are to be considered to be expressly stated in this application. Numerical ranges have been recited, as discussed herein, in reference to density, melt index, weight percent of component and other properties.


The term “polymer” is used herein to indicate, a homopolymer, a copolymer, or a terpolymer. The term “polymer” as used herein includes interpolymers, such as those made by the copolymerization of ethylene with C3-C10 alpha olefins or polypropylene with C4-C10 alpha olefins.


The term “interpolymer,” as used herein, refers to polymers prepared by the polymerization of at least two different types of monomers. The generic term interpolymer thus includes copolymers, usually employed to refer to polymers prepared from two different types of monomers, and polymers prepared from more than two different types of monomers.


The term “ethylene-based interpolymer,” as used herein, refers to an interpolymer that contains at least a majority mole percent ethylene (greater than 50 mole percent, based on total amount (moles) of polymerizable monomer), and one or more additional comonomers.


The term “ethylene/α-olefin interpolymer,” as used herein, refers to an ethylene-based interpolymer that contains at least a majority mole percent ethylene (greater than 50 mole percent, based on total amount (moles) of polymerizable monomer), an α-olefin, and optionally, one or more additional comonomers.


The term “single peak,” in reference to an ATREF profile, refers to a peak which does not exhibit two or more distinct maxima. Such a peak may have a leading tail.


The term “unimodal” as used herein in reference to the overall MWD of comparative examples, or in reference to the MWD of a component polymer of the inventive composition, means the MWD in a Gel Permeation Chromatography (GPC) curve does not substantially exhibit multiple component polymers, that is, no humps, shoulders or tails exist or are substantially discernible in the GPC curve. In other words, the DOS (Degree of Separation) is zero or substantially close to zero.


The term “bimodal” as used herein means that the MWD in a GPC curve exhibits two component polymers wherein one component polymer may even exist as a hump, shoulder or tail relative to the MWD of the other component polymer.


The term “multimodal” as used herein means that the MWD in a GPC curve exhibits more than two component polymers wherein one component polymer may even exist as a hump, shoulder or tail relative to the MWD of the other component polymer.


The term “distinct” as used in reference to the MWD of the LMW component and the HMW component means there is no substantial overlapping of the two corresponding molecular weight distributions in the resulting GPC curve. That is, each molecular weight distribution is sufficiently narrow and their average molecular weights are sufficiently different that the MWD of both components substantially exhibits a baseline on its HMW side as well as on its LMW side. In other words, the DOS is at least 1, preferably at least 2, 4, 5, 7, 9, or 10.


The term “catalyst precursor” as used herein means a mixture comprising titanium and magnesium compounds and a Lewis Base electron donor.


The term “inertly substituted” refers to substitution with atoms or groups which do not undesirably interfere with the desired reaction(s) or desired properties of the resulting coupled polymers.


The term LTD used herein refers to the distribution of the lamella thickness, Lc, of a polymer.


The term “substantially singular peak” is used herein with reference to LTD curves to mean that a peak does not substantially exhibit two or more peaks. But a “substantially single peak” may not follow a Gaussian distribution, may be broader than a Gaussian distribution would indicate, or have a flatter peak than a Gaussian distribution. Some substantially singular peaks may have a tail on either side of the peak. In some embodiments it may be possible to mathematically resolve a “substantially single peak” in an LTD curve into two or more components by various methods. In some embodiments a “substantially single peak” in an LTD curve follows the equation:













P
H

-

P
L



P
i


×
100





%







10

%





(
1
)









    • where Pi is a point in the LTD curve having a value for the percent weight fraction between that of the highest weight fraction value, PH, of the LTD trace and the lowest point, PL, having an Lc value between the Lc value of Pi and the Lc value of PH. In some instances, this percent difference is less than about 8%, or less than about 7%. In some embodiments a substantially single peak has a difference of about 5% or less or about 2.5% or less. Of course in some embodiments, there is no point PL between Pi and PH so the percent difference is zero.





As used herein, the term “rheology modification” means change in melt viscosity of a polymer as determined by creep measurements and Dynamic Mechanical spectroscopy (DMS).


The term “melt processing” is used to mean any process in which the polymer is softened or melted, such as extrusion, pelletizing, film blowing and casting, thermoforming, compounding in polymer melt form, and the like.


The term “extruder” is used for its broadest meaning to include such devices, as a device which extrudes pellets or pelletizer.


The terms “blend” or “polymer blend,” as used herein, mean a blend of two or more polymers. Such a blend may or may not be miscible. Such a blend may or may not be phase separated. Such a blend may or may not contain one or more domain configurations, as determined from transmission electron microscopy, light scattering, x-ray scattering, and other methods known in the art.


Test Methods


Density


Resin density was measured by the Archimedes displacement method, ASTM D 792-03, Method B, in isopropanol. Specimens were measured within 1 hour of molding, after conditioning in the isopropanol bath at 23° C. for 8 minutes to achieve thermal equilibrium prior to measurement. The specimens were compression molded according to ASTM D-4703-00, Annex A, with a 5 min initial heating period at about 190° C. (±2° C.) and a 15° C./min cooling rate per Procedure C. The specimen was cooled to 45° C. in the press, with continued cooling until “cool to the touch.”


Flexural and Secant Modulus Properties


The resin stiffness is characterized by measuring the Flexural Modulus at 5% strain and Secant Modulii at 1% and 2% strain, and a test speed of 0.5 inch/min (13 mm/min) per ASTM D 790-03 Method B. The specimens are compression molded according to ASTM D-4703-00 Annex 1, with a 5 min initial heating period at about 190° C. (±2° C.), and a 15° C./min cooling rate per Procedure C. The specimen is cooled to 45° C. in the press with continued cooling until “cool to the touch.


Tensile Properties


Tensile strength at yield, elongation at yield, tensile strength at break, and elongation at break are measured according to ASTM D-638-03, with a test speed of two inches per minute. All measurements are performed at 23° C. on rigid type IV specimens, which are compression molded per ASTM D 4703-00, Annex A-1, with a 5 minute initial heating period at about 190° C. (±2° C.), and a 15° C./min cooling rate per Procedure C. The specimen is cooled to 45° C. in the press, with continued cooling until “cool to the touch.”


Melt Flow Rate by Extrusion Plastomer


Melt flow rate measurements were performed according to ASTM D-1238-04, Condition 190° C./2.16 kg and Condition 190° C./21.6 kg, which are known as I2 and I21, respectively. Melt flow rate is inversely proportional to the molecular weight of the polymer. Thus, the higher the molecular weight, the lower the melt flow rate, although the relationship is not linear. Melt Flow Ratio (MFR) is the ratio of melt flow rate (I21) to melt flow rate (I2), unless otherwise specified.


When polymers are tested with fluoroelastomer processing aide, the melt indexer should be thoroughly cleaned after each use.


Polymer Fines


The amount of polymer fines in a given sample was determined using the following method: 500 grams of polymer were added to a standard sieve set consisting of the following US mesh sizes: 10, 18, 35, 60, 120, 200 (2000 μm, 1000 μm, 500 μm, 250 μm, 125 μm, 75 μm) and pan. A Rotap or Gradex 2000 shaker was used to separate the particles. The materials which pass through the 120 mesh screen and remain on the pan were classified as fines. The geometric mean is used to calculate the particle average particle size (APS).


Bulk Density


Bulk density of the polymer was determined using ASTM D1895-96 (re-approved 2003).


Film Appearance Rating (FAR)


A FAR value is obtained by comparing the extruded film to a set of reference film standards, both at 1.5 mil (38 μm) thickness for the pipe and blow molding resins. The film resin is fabricated to 1 mil thickness (25 μm) and compared to the 1.5 mil (38 μm) film standards. The standards are available from The Dow Chemical Company (Test Method PEG #510 FAR). For all resins except film resins, the following method is used. The resin extruded is pelleted resin which includes the stabilizer(s). A Model CE-150-20, 38 mm (1.5 in) 20:1 L/D, MPM Custom Equipment electrically heated air-cooled extruder with 7 heating zones (3 barrel, 1 gate, 3 die) is used to make the film specimens.


A more detailed extruder description is as follows:

    • Extruder Manufacturer: MPM Polymer Systems, Inc.
      • Type: Low Boy [610 mm (24 in) Center Line]
      • Heating: Electrical 425° C. controllers
      • Cooling: Only on hopper (water)
      • Speed: Variable
    • Screw Manufacturer: MPM Polymer Systems, Inc.
      • Type: 20:1 standard low density polyethylene screw bored to midway of transition section.
      • Diameter: 38 mm (1.5 in)
      • L to D: 20/1
    • Die Manufacturer: MPM Polymer Systems, Inc.
      • Diameter: 100 mm (4 in)
      • Gap: 30 mil (0.762 mm)
      • Type: Deep Side Fed
    • Blower Manufacturer: Buffalo Forge
      • Air flow control damper on suction
      • Air flow control valving on discharge
      • Motor: 1.5 hp (1120 W), 2 speeds
      • Air equalizing chamber between blower and air
    • Air Ring Manufacturer: MPM Polymer Systems, Inc.
      • Layout 708
      • Diameter: 172 mm (6.75 in) I.D.
      • Type: Adjustable lip
    • Tower Height: 914 mm (36 in)
    • Collapsing Frame Length: 343 mm (13.5 in)


The extrusion conditions for the FAR test were as follows:

    • Screw Neutral
    • Hopper Water Full Flow
    • Temperatures (° C.)


















Zone 1
210



Zone 2
210



Zone 3
210



Gate
225



Adapter
225



Die Zone 1
225



Die Zone 2
225



Screen Pack, stainless steel, mesh
40/40












    • Output:

















Output:











Screw Speed
65
rpm










Blow up Ratio
2/1











Lay flat width
12 in
(304.8 mm)



Frost Line Height
103 in
(254 mm)



Tower Height
36 in
(914.4 mm)







Film Rating Test:











Nip Roll Speed
254 ft/min
(1.29 m/s)



Film Gauge
1.5 mil
(0.038 mm)



Range for Film Gauge
1.3-1.7 mil
(33-43.2 μm)










The screw speed can be adjusted to give proper throughput rates. Frost line is measured from the lower level of the air ring. The nip roll speed is varied until a film thickness of 1.5 mil (38 μm) was obtained. Film thickness is measured using a Federal dial indicator gauge according to ASTM D 374.


After the extruder has reached thermal equilibrium, and uniform film is being produced, a film sample of 3 m length is taken. Ratings are based upon the worst section viewed in each sample. This rating is based on the level of gels observed in the film, a general term for a discrete imperfection in polyethylene film. Gels may be formed from high molecular weight material, either clear or discolored, lint or other foreign contamination, or resin cross contamination. Gels are the most common defect encountered in films, and account for a large portion of the film rating. Other defects were noted, but normally are not included in the film appearance value. If needed, reference is made to a set of high density film standards during this evaluation. The values given are in increments of 10 units ranging from +50 (best) to −50 (worst).


Lamellar Thickness Distribution (LTD)


An LTD curve refers to a plot of the weight percent as a function of the lamellar thickness (Lc). Additional information can be found in U.S. Pat. No. 4,981,760 and U.S. Publication 2004/0034169 A1, which are incorporated by reference herein in their entireties.


The LTD data are obtained and analyzed in the following manner. Samples are cut directly from the fabricated polyethylene products. DSC samples are taken from the pipe wall, film, or plaques used for PENT measurements. Samples can also be taken from the pellets to gain an insight into the effect of pelletizing conditions on LTD. If the fabrication process did not yield a uniform cooling/solidification profile, samples are taken from different parts of the product to reflect these differences. This may be important in extruded pipes if the pipe was cooled from the outside to the inside by cold water such that the cooling rate therefore decreased from the outside to the inside of the pipe wall. To reflect these differences, at least three samples are taken from the outside, middle and inside layer of the pipe wall. About 10 mg of sample is analyzed by DSC using a heating rate of 10° C./min. To better compare the differences caused by molecular variables, the solidification history of the sample is standardized as follows: the specimen is recrystallized by melting the specimen in the DSC sample holder at 190° C., and then cooled down to 30° C. at the rate of 20° C./min to eliminate artifacts in the DSC curve that might otherwise be observed due to previous fabrication processes.


A three step procedure is used. First, the LTD in products, such as pipes or film, is determined by scanning the sample from 30° C. to 190° C. at the heating rate of 10° C./min. The characteristic of the resultant LTD is associated with both the material variables and the processing condition. The sample is maintained at 190° C. for one minute to completely relax the molecular chains. Second, the sample is cooled at the cooling rate of 20° C./min, from 190° C. to 30° C., to allow the sample to re-crystallize under controlled conditions. The temperature is maintained at 30° C. for one minute. Third, the sample is heated at a rate of 10° C./min to determine LTD in the re-crystallized sample. This LTD is used to investigate the effect of material variables by eliminating the fabrication factors. First, the DSC melting peak is integrated. The melting temperature and the corresponding integrated partial area of the melting peak were recorded. The melting temperature is then used to calculate the lamella thickness, 1, of polyethylene crystal according to the well-known Thomson-Gibbs equation from the melting point, Tm.











T
m

=


T
m


(

1
-


2






σ
e



ℓ•Δ






h
m




)


,




(
1
)







where Tmo is the equilibrium melting point of an infinite crystal, σe is the surface free energy of the basal plane, and Δhm is the enthalpy of fusion per unit volume. In Die Makromolekulare Chemie, 1968, 113, 1-22, Illers and Hendus experimentally determined the constants in equation (1). The lamella thickness, Lc (nm), then can be calculated from the melting point, Tm (K).










L
c

=



0.62
-
414.2


414.2
-

T
m



.





(
2
)







For a given melting temperature from the DSC melting peak, the corresponding lamella thickness is obtained from equation (2). Lamellar thickness distributions are also discussed in Polymer vol. 38, issue 23 (1997) by Zhou, Hongi, and Wilkes, the disclosure of which is hereby incorporated by reference. The integrated partial area of the melting peak is used to calculate the differentiated weight percent of the crystal for a given lamella thickness. The partial area, ΔHi, of a DSC melting peak is assumed to be proportional to the weight percent of the lamella crystal within this partial area. The differentiated weight percent, wt %, of the lamellae at the thickness Lc,i is therefore determined by equation (3).










wt





%






(

L

c
,
i


)


=






(

Δ






H
i


)


/
Δ







H
total





(

L
c

)







(
3
)







The plot of the weight percent from the integrated partial area as a function of the lamella thickness gives the LTD curve. In addition, the total heat fusion of the melting peak can be used to determine the crystallinity. The detailed data analysis process is discussed in the following. Analysis of the LTD curve obtained from the procedure described above can be analogized to the analysis of (MWD) or polydispersity index (PDI) based on the weight (Mw) and number (Mn) average molecular weight, the thickness average, Lt, and number average, Ln, lamella thickness are therefore defined by equation (4) and (5).










L
t

=






i
=
1






L

c
,
i

2



n
i







i
=
1






L

c
,
i




n
i




=




i
=
1






L

c
,
i



Δ







H
i

/
Δ






H







(
4
)







L
c

=






i
=
1






L

c
,
i




n
i







i
=
1





n
i



=

1




i
=
1






(


Δ






H
i



Δ





H


)

/

L

c
,
i










(
5
)







Similar to the polydispersity index (PDI=MWD=Mw/Mn) which gives information regarding the molecular weight distribution, the lamella dispersity index, LDI, is hence given by equation









LDI
=



L
t


L
n


.





(
6
)







Thus, the LDI is a quantitative characteristic of the breadth of the LTD curve.


Differential Scanning Calorimetry (DSC)


Thermal measurements, Tm and Tc, are generated via a TA Instruments Model Q1000 DSC, equipped with an RCS (refrigerated cooling system) cooling accessory and an auto sampler. A nitrogen purge gas flow of 50 ml/min is used throughout. The sample is pressed into a thin film, using a press at 175° C. and 1500 psi (10.3 MPa) maximum pressure, for about 15 seconds, then air-cooled to room temperature at atmospheric pressure. About 3 to 10 mg of material is then cut into a 6 mm diameter disk using a paper hole punch, weighed to the nearest 0.001 mg, placed in a light aluminum pan (ca 50 mg) and then crimped shut.


The thermal behavior of the sample is investigated with the following temperature profile. The sample was rapidly heated to 180° C., and held isothermal for 3 minutes, in order to remove any previous thermal history. The sample is then cooled to −40° C. at 10° C./min cooling rate, and is held at −40° C. for three minutes. The sample is then heated to 150° C. at 10° C./min heating rate. The cooling and second heating curves are recorded.


Gel Permeation Chromatography (GPC)


The following procedure was used to determine the molecular architecture of various polymer compositions. The chromatographic system consisted of a Waters (Millford, Mass.) 150° C. high temperature gel permeation chromatograph, equipped with a Precision Detectors (Amherst, Mass.) 2-angle laser light scattering detector Model 2040. The 15° angle of the light scattering detector was used for calculation purposes. Data collection was performed using Viscotek TriSEC software version 3 and a 4-channel Viscotek Data Manager DM400. The system was equipped with an on-line solvent degas device from Polymer Laboratories.


The carousel compartment was operated at 140° C., and the column compartment was operated at 150° C. The columns used were four Shodex HT 806M 300 mm, 13 μm columns and one Shodex HT803M 150 mm, 12 μm column. The solvent used was 1,2,4-trichlorobenzene. The samples were prepared at a concentration of 0.1 grams of polymer in 50 milliliters of solvent. The chromatographic solvent and the sample preparation solvent contained 200 μg/g of butylated hydroxytoluene (BHT). Both solvent sources were nitrogen sparged. Polyethylene samples were stirred gently at 160° C. for 4 hours. The injection volume used was 200 microliters and the flow rate was 0.67 milliliters/min.


Calibration of the GPC column set was performed with 21 narrow molecular weight distribution polystyrene standards with molecular weights ranging from 580 to 8,400,000 g/mol which were arranged in six “cocktail” mixtures with at least a decade of separation between individual molecular weights. The standards were purchased from Polymer Laboratories (Shropshire, UK). The polystyrene standards were prepared at 0.025 grams in 50 milliliters of solvent for molecular weights equal to, or greater than, 1,000,000 g/mol, and 0.05 grams in 50 milliliters of solvent for molecular weights less than 1,000,000 g/mol. The polystyrene standards were dissolved at 80° C. with gentle agitation for 30 minutes. The narrow standards mixtures were run first, and in order of decreasing highest molecular weight component to minimize degradation. The polystyrene standard peak molecular weights were converted to polyethylene molecular weights using equation 8 (as described in Williams and Ward, J. Polym. Sci., Polym. Let., 6, 621 (1968)):

Mpolyethylene=A×(Mpolystyrene)B  (8),

where M is the molecular weight, A has a value of 0.41 and B is equal to 1.0.


The Systematic Approach for the determination of multi-detector offsets was done in a manner consistent with that published by Balke, Mourey, et al. (Mourey and Balke, Chromatography Polym. Chpt 12, (1992) and Balke, Thitiratsakul, Lew, Cheung, Mourey, Chromatography Polym. Chpt 13, (1992)), optimizing dual detector log results from Dow broad polystyrene 1683 to the narrow standard column calibration results from the narrow standards calibration curve using in-house software.


The molecular weight data for off-set determination was obtained in a manner consistent with that published by Zimm (Zimm, B. H., J. Chem. Phys., 16, 1099 (1948)) and Kratochvil (Kratochvil, P., Classical Light Scattering from Polymer Solutions, Elsevier, Oxford, N.Y. (1987)). The overall injected concentration used for the determination of the molecular weight was obtained from the sample refractive index area and the refractive index detector calibration from a linear polyethylene homopolymer of 115,000 g/mol molecular weight, which was measured in reference to NIST polyethylene homopolymer standard 1475. The chromatographic concentrations were assumed low enough to eliminate addressing 2nd Virial coefficient effects (concentration effects on molecular weight).


Molecular weight calculations were performed using in-house software. The calculation of the number-average molecular weight, weight-average molecular weight, and z-average molecular weight were made according to the following equations assuming that the refractometer signal is directly proportional to weight fraction. The baseline-subtracted refractometer signal can be directly substituted for weight fraction in the equations below. Note that the molecular weight can be from the conventional calibration curve or the absolute molecular weight from the light scattering to refractometer ratio. An improved estimation of z-average molecular weight, the baseline-subtracted light scattering signal can be substituted for the product of weight average molecular weight and weight fraction in equation (9) below:



















a
)







Mn
_


=




i



Wf
i





i



(


Wf
i

/

M
i


)













b

)







Mw
_


=




i



(


Wf
i

*

M
i


)





i



Wf
i













c

)













Mz
_


=





i



(


Wf
i

*

M
i
2


)





i



(


Wf
i

*

M
i


)



.





(
9
)







The term “bimodal,” as used herein, means that the MWD in a GPC curve exhibits two component polymers, wherein one component polymer may even exist as a hump, shoulder or tail relative to the MWD of the other component polymer. A bimodal MWD can be deconvoluted into two components: LMW component and HMW component. After deconvolution, the peak width at half maxima (WAHM) and the average molecular weight (Mw) of each component can be obtained. Then the degree of separation (DOS) between the two components can be calculated by equation 10:










DOS
=



log


(

M
w
H

)


-

log


(

M
w
L

)





WAHM
H

+

WAHM
L




,




(
10
)








wherein MwH and MwL are the respective weight average molecular weight of the HMW component and the LMW component; and WAHMH and WAHML the respective peak width at the half maxima of the deconvoluted molecular weight distribution curve for the HMW component and the LMW component.


The DOS for the new composition is about 0.01 or higher. In some embodiments, DOS is higher than about 0.05, 0.1, 0.5, or 0.8. Preferably, DOS for the bimodal components is at least about 1 or higher. For example, DOS is at least about 1.2, 1.5, 1.7, 2.0, 2.5, 3.0, 3.5, 4.0, 4.5, or 5.0. In some embodiments, DOS is between about 5.0 to about 100, between about 100 to 500, or between about 500 to 1,000. It should be noted that DOS can be any number in the above range. In other embodiments, DOS exceeds 1,000.


Swell


The resin swell is measured by the Dow Lab Swell method which consists of measuring the time required by an extruded polymer strand to travel a pre-determined distance of 230 mm. The Göttfert Rheograph 2003 with, 12 mm barrel, and equipped with a 10 L/D capillary die is used for the measurement. The measurement was carried out at 190° C., at two fixed shear rates, 300 s−1 and 1,000 s−1, respectively. The more the resin swells, the slower the free strand end travels and, the longer it takes to cover 230 mm. The swell is reported as t300 and t1000 (s) values.


Rheology


The sample is compression molded into a disk for rheology measurement. The disks are prepared by pressing the samples into 0.071″ (1.8 mm) thick plaques, and were subsequently cut into 1 in (25.4 mm) disks. The compression molding procedure is as follows: 365° F. (185° C.) for 5 min at 100 psi (689 kPa); 365° F. (185° C.) for 3 min at 1500 psi (10.3 MPa); cooling at 27° F. (15° C.)/min to ambient temperature (about 23° C.).


The resin rheology is measured on the ARES I (Advanced Rheometric Expansion System) Rheometer. The ARES is a strain controlled rheometer. A rotary actuator (servomotor) applies shear deformation in the form of strain to a sample. In response, the sample generates torque, which is measured by the transducer. Strain and torque are used to calculate dynamic mechanical properties such as modulus and viscosity. The viscoelastic properties of the sample are measured in the melt using a parallel plate set up, at constant strain (5%) and temperature (190° C.), and as a function of varying frequency (0.01 to 100 or 500 s−1). The storage modulus (G′), loss modulus (G″), tan delta, and complex viscosity (eta*) of the resin are determined using Rheometrics Orchestrator software (v. 6.5.8).


Low shear rheological characterization is performed on a Rheometrics SR5000 in stress controlled mode, using a 25 mm parallel plates fixture. This type of geometry is preferred to cone and plate because it requires only minimal squeezing flow during sample loading, thus reducing residual stresses.


Creep measurements are carried out at 170° C. and 190° C. After zeroing the gap between the parallel plates, the temperature is increased to 220° C. for sample loading (about 5 min) in order to accelerate the relaxation of normal stresses, and then decreased to the measuring temperature. Creep test was performed under a stress of 20 Pa, which is the best compromise to have a good signal to noise (S/N) ratio, while remaining in the linear (low deformation) regime. The deformation is recorded with time up to 30,000 s, or until the viscosity leveled off, indicating that the steady state is reached. The steady-state viscosity is determined using the automatic feature of the Rheometrics Orchestrator software (v. 6.5.8). Several repeats were run, until the standard deviation on the steady-state viscosity decreased below 4%.


A Dynamic Mechanical Spectroscopy (DMS), also called frequency sweep, test in stress-controlled mode is performed before and after the first creep run to check for degradation. The angular frequency is varied from 0.1 to 100 rad/s with a stress amplitude of 1000 Pa, which corresponds to strain amplitudes between 0.1% (at 100 rad/s) and 10% (at 0.1 rad/s). It is concluded that stability is good. On the subsequent runs, the DMS test is run only after the creep test to avoid introducing perturbations due to shear history.


The steady-state data point from creep is combined with the viscosity curve from DMS to extend the accessible range of shear rates down to 10-61/s, and fitted with the 4-parameter Carreau-Yasuda model:

η=c1(1+(c2x)c3)(c4−1)/c3  (11).

Antioxidant Content by High Pressure Liquid Chromatography (HPLC)


Antioxidants, such as Irgafos 168 and Irganox 1010, are commonly used to protect the polymer from thermal and or oxidative degradation. Irganox 1010 is tetrakis (methylene (3,5 di tert-butyl-4-hydroxyhydrocinnamate) available from Ciba Geigy Inc. Irgafos 168 is tris-(2,4-di-tert-butylphenyl) phosphite available from Aldrich Chemical Company.


Sample Preparation: Polyolefin pellets are powdered using a Retsch Model ZM100 Grinder fitted with a 1.0 mm sieve. The 1.0 mm sieve produces particles with an average size of 0.5 mm. The pellets and grinder are chilled with liquid nitrogen prior to grinding. About 2 grams of polymer is placed in a polystyrene cup, and about 50 mL of liquid nitrogen is added to cool the polymer. About 50 mL of liquid nitrogen is poured into the funnel of the grinder to cool the mechanical parts, followed by pouring the liquid and the pellets from the polystyrene cup into the grinder.


Extraction: Five grams of the powder is extracted with 40 mls of carbon disulfide (C2S) by shaking with an automated shaker for 72 hours. Five mls of the extract ware taken from the clear, transparent lower layer of the CS2 extract and dried under a gently flowing dry nitrogen stream. The resulting residue is dissolved in 5 ml of isopropanol, with gentle heating on a steam bath, cooled and filtered using a 0.2 m syringe filter into a HPLC sample vial, and analyzed by HPLC according to the following procedure.


The HPLC instrument is a HP 1090 available from Hewlett-Packard, Inc., with a Thermo Hypersil column from Keystone Scientific. The column packing is Waters Spherisorb ODS 2. Column size was 150×4.6 mm, pore size 80 {dot over (a)}ngströms, and particle size 3 μm. The initial solvent is a mixture consisting of 30% water and 70% acetonitrile. At 10 minutes, 100% acetonitrile is introduced, then at 15 minutes a mixture consisting of 80% acetonitrile and 20% isopropanol is introduced. Total run time is 20 minutes at a flow rate of 1 ml per minute. The 276 nm wavelength is monitored.


Calibration for each additive is performed by making up a known concentration of the additive in isopropanol (about 0.03 g per 100 ml). For oxidized Irgafos 168 the calibration is performed by oxidizing a standard isopropanol solution of Irgafos 168 with excess hydrogen peroxide for one hour.


Brittleness Temperature


Brittleness temperature is measured according to ASTM D-746, Procedure A, using a Tinius Olsen Brittle Point Tester, with specimen Type 1, for fixture type A, tightened with torque per Note 8. Heat transfer medium is methanol or isopropanol.


Thermal Stability


Thermal Stability is measured according to ASTM D-3350-02, section 10.1.9, by a DSC technique. Thermal Stability is also called Oxidation Induction Time, with the time to failure measured at 210° C. Test specimens taken from pipe or fittings made from the virgin material are measured using differential scanning calorimeter (DSC). The directions of the instrument (DSC) manufacturer regarding calibration and operation is followed, except when in conflict with other parts of section 10.1.9. The polyethylene-based resin contains sufficient antioxidant, so that the minimum induction temperature is 220° C., when tested in accordance with section 10.1.9.


The g′ Average


The g′ is expressed as the ratio of intrinsic viscosity of the instant high-density polyethylene composition to the intrinsic viscosity of a linear polymer reference. The g′ average was determined according to the following procedure.


The chromatographic system consisted of a Waters (Millford, Mass.) 150° C. high temperature chromatograph, equipped with a Precision Detectors (Amherst, Mass.) t-angle laser light scattering detector Model 2040, an IR4 infra-red detector from Polymer Char (Valencia, Spain), and a Viscotek (Houston, Tex.) 150R 4-capillary viscometer. The 15-degree angle of the light scattering detector was used for calculation purposes. Data collection was performed using Viscotek TriSEC software, version 3, and a 4-channel Viscotek Data Manager DM400. The system was equipped with an on-line solvent degas device from Polymer Laboratories. The carousel compartment was operated at 140° C., and the column compartment was operated at 150° C. The columns used were 4, 20-micron mixed-bed light scattering “Mixed A-LS” columns from Polymer Laboratories. The solvent used was 1,2,4-trichlorobenzene. The samples were prepared at a concentration of 0.1 grams of polymer in 50 milliliters of solvent. The chromatographic solvent and the sample preparation solvent contained 200 ppm of butylated hydroxytoluene (BHT). Both solvent sources were nitrogen sparged. Polyethylene samples were stirred gently at 160 degrees Celsius for 4 hours. The injection volume used was 200 microliters, and the flow rate was 1 milliliters/minute.


Calibration of the GPC column set was performed with 21 narrow molecular weight distribution polystyrene standards, with molecular weights ranging from 580 to 8,400,000, and were arranged in 6 “cocktail” mixtures with at least a decade of separation between individual molecular weights. The standards were purchased from Polymer Laboratories (Shropshire, UK). The polystyrene standards were prepared at 0.025 grams in 50 milliliters of solvent for molecular weights equal to, or greater than, 1,000,000, and 0.05 grams in 50 milliliters of solvent for molecular weights less than 1,000,000. The polystyrene standards were dissolved at 80° C., with gentle agitation for 30 minutes. The narrow standards mixtures were run first, and in order of decreasing highest molecular weight component to minimize degradation. The polystyrene standard peak molecular weights were converted to polyethylene molecular weights using the following equation (as described in Williams and Ward, J. Polym. Sci., Polym. Let., 6, 621 (1968)).:

Mpolyethylene=A×(Mpolystyrene)B

Where M is the molecular weight, A has a value of 0.43 and B is equal to 1.0.


The Systematic Approach for the determination of multi-detector offsets was done in a manner consistent with that published by Balke, Mourey, et. al. (Mourey and Balke, Chromatography Polym. Chpt 12, (1992)) (Balke, Thitiratsakul, Lew, Cheung, Mourey, Chromatography Polym. Chpt 13, (1992)), optimizing triple detector log(MW and IV) results from Dow Broad Polystyrene 1683 to the narrow standard column calibration results from the narrow standards calibration curve using a software. The molecular weight data for off-set determination was obtained in a manner consistent with that published by Zimm (Zimm, B. H., J. Chem. Phys., 16, 1099 (1948)) and Kratochvil (Kratochvil, P., Classical Light Scattering from Polymer Solutions, Elsevier, Oxford, N.Y. (1987)). The overall injected concentration used for the determination of the molecular weight was obtained from the sample refractive index area and the refractive index detector calibration from a linear polyethylene homopolymer of 115,000 molecular weight. The chromatographic concentrations were assumed low enough to eliminate addressing 2nd Virial coefficient effects (concentration effects on molecular weight).


The g′ average was calculated for the samples as follow:


1. Calibrated the light scattering, viscosity, and concentration detectors with NBS1475 homopolymer polyethylene (or equivalent reference);


2. Corrected the light scattering and viscometer detector offsets relative to the concentration detector as described in the calibration section;


3. Subtracted baselines from the light scattering, viscometer, and concentration chromatograms and set integration windows making certain to integrate all of the low molecular weight retention volume range in the light scattering chromatogram that were observable from the refractometer chromatogram;


4. Established a linear homopolymer polyethylene Mark-Houwink reference line by injecting a standard with a polydispersity of at least 3.0, calculated the data file (from above calibration method), and recorded the intrinsic viscosity and molecular weight from the mass constant corrected data for each chromatographic slice;


5. Injected the HDPE sample of interest and calculated the data file (from above calibration method), and recorded the intrinsic viscosity and molecular weight from the mass constant corrected data for each chromatographic slice;


6. Shifted the homopolymer linear reference intrinsic viscosity by the following factor: IV=IV+1/(1+2*SCB/1,000C*branch point length) where IV is the intrinsic viscosity of the HDPE sample of interest, SCB/1,000C was determined from C13 NMR, and the branch point length is 2 for butene, 4 for hexene, or 6 for octene);


7. Calculated g′ average according to the following equation.







g


=







j
=


Where





M

>
40


,
000

HighestM



[


c
j

×


(


IV
j


IV
Lj


)

M


]


+




j
=
LowestM



WhereM
>
40

,
000




c
j







j
=

Lowest





M


HightestM



c
j







In the above equation, c is the concentration of the slice, IV is the intrinsic viscosity of the HDPE, and IVL is the intrinsic viscosity of the linear homopolymer polyethylene reference (corrected for SCB of the HDPE sample of interest) at the same molecular weight (M). The IV ratio was assumed to be one, at molecular weights less than 40,000 to account for natural scatter in the light scattering data.


The polyethylene composition may have a g′ average of equal, or greater than, 1, as measured by Triple Detector GPC, as described above. As discussed above, the g′ is expressed as the ratio of intrinsic viscosity of the instant high-density polyethylene composition to the intrinsic viscosity of a linear polymer reference. If the g′ is equal, or greater than, 1, then the sample being analyzed is considered linear, and if g′ is less than 1, it is, then, by definition a branched polymer as compared to a linear polymer. However, current testing methods may be subject to errors in their precision and accuracy; thus, proper steps must be taken to account for such precision errors. Therefore, small deviations, for example values of less than, or equal to, 0.012, from unity, i.e. 0.988 would still be defined as linear polymers.


Film Property Measurements


Tear resistance values were obtained using an Elmendorf Tear Tester in compliance with the ASTM D-1922-06a. For each film sample, ten to fifteen specimens were tested in both machine (MD) and transverse/cross (TD/CD) direction.


Dart impact testing was measured according to ASTM D 1709-04, Method A, and Method B, if there were no failures via Method A, by the staircase technique, with the dart dropped around the circumference of the film sample, using film specimens with the appropriate thickness. The specimens were taken from a blown film line, after at least three minutes of blowing the film with a clean die lip to avoid scratches. The films were aged at standard laboratory conditions of 23° C. and 50% relative humidity, for a period of at least 40 hours. Test Methods A and B are used to establish the weight of the dart when 50% of the test specimens fail under the specified conditions.


Test Method A employs a dart with a 38.10±0.13 mm (1.500±0.005 in) diameter hemispherical head, dropped from a height of 0.66±0.01 m (26.0±0.4 in). This test method may be used for films, whose impact resistance requires masses of about 50 g, or less, to about 2 kg, to impart fracture.


Test Method B employs a dart with a 50.80±0.13 mm (2.000±0.005 in) diameter hemispherical head, dropped from a height of 1.50±0.03 m. Its range of applicability is from about 0.3 kg to about 2 kg.


The impact resistance cannot be normalized over a range of thickness, since no simple correlation exists between film thickness and impact resistance. Data from these test methods are comparable only for test specimens that vary by no more than ±25% from the nominal or average thickness of the specimens tested.


Film tensile properties were measured according to ASTM D-882-02.


Film gloss was measured according to ASTM D-2457-03 (45 degree gloss).


Film haze was measured according to ASTM D-1003-00 (Method A).


Film puncture resistance was measured according to ASTM D-5748-07.


Film COF O/I was measured according to ASTM D-1894-06.


The following examples are provided for the purpose of illustrating the invention, and are not to be construed as limiting the scope of the invention.


Examples of the Invention

The following examples are to illustrate this invention and to not limit it. Ratios, parts, and percentages are by weight, unless otherwise stated.


Inventive Samples: I922; I515; I516; I513; I514; I517; and D20.


Comparative Samples: C918; C919; C920; C921; C923; C924; C636; C024; C025; C453; C454; C586; C587; C588; C589; C590; C591; C592; C510; C512.


Competitive Samples: COM049; and COM769.


ATREF-DV profiles of several compositions are shown in FIGS. 1-29.


Catalyst Preparation


Preparation of Catalyst Precursor


For the inventive and comparative examples, a titanium trichloride catalyst precursor was prepared in an approximately 7,500 liter glass lined vessel, equipped with pressure and temperature control, and a turbine agitator. A nitrogen atmosphere (<5 ppm H2O) was maintained at all times. Tetrahydrofuran (10,500 lbs, 4,800 kg, <400 ppm H2O) was added to the vessel. The tetrahydrofuran was recovered from a closed cycle dryer, and contained approximately 0.1 percent Mg and 0.3 percent Ti. An “11 percent THF solution” of triethylaluminum was added to scavenge residual water. The reactor contents were heated to 40° C., and 13.7 lbs (6 kg) of granular magnesium metal (particle size 0.1-4 mm) was added, followed by 214.5 lbs (97.3 kg) of titanium tetrachloride added over a period of one-half hour.


The mixture was continuously agitated. The exotherm resulting from the addition of titanium tetrachloride caused the temperature of the mixture to rise to approximately 44° C. The temperature was then raised to 70° C., and held at that temperature for approximately four hours, then cooled to 50° C. At the end of this time, 522 pounds (238 kg) of magnesium dichloride were added, and heating initiated to raise the temperature to 70° C. The mixture was held at this temperature for another five hours, then cooled to 35° C., and filtered through a 100 mesh (150 μm) filter to remove solids.


Fumed silica (CAB-O-SIL™ TS-610, manufactured by the Cabot Corporation) (811 lbs, 368 kg) was added to the above precursor solution over a period of one hour. The mixture was stirred by means of a turbine agitator during this time, and for 4 hours thereafter, to thoroughly disperse the silica. The temperature of the mixture was held at 40° C. throughout this period, and a dry nitrogen atmosphere was maintained at all times. The resulting slurry was spray dried using an 8-foot diameter closed cycle spray dryer, equipped with a rotary atomizer. The rotary atomizer was adjusted to give catalyst particles with a D50 on the order of 20-30 μm. The scrubber section of the spray dryer was maintained at approximately +5 to −5° C.


Nitrogen gas was introduced into the spray dryer at an inlet temperature of 140 to 165° C., and was circulated at a rate of approximately 1000-1800 kg/hour. The catalyst slurry was fed to the spray dryer at a temperature of about 35° C., and a rate of 65-150 kg/hour, or sufficient to yield an outlet gas temperature in the range of 100-125° C. The atomization pressure was maintained at slightly above atmospheric. The resulting catalyst particles were mixed with mineral oil (Kaydol™ 350, available from Witco Corporation), under a nitrogen atmosphere in a 400 liter glass lined vessel, equipped with a turbine agitator, to form a slurry containing approximately 28 percent of the catalyst precursor.


Catalyst Precursor Partial Pre-activation


In some of the polymerizations (noted 0017 reduction), the catalyst precursor was partially pre-activated. The mineral oil slurry of precursor was partially activated by contact at room temperature with a 30 percent mineral oil solution of diethylaluminum chloride (DEAC), a 50 percent mineral oil solution of tri-n-hexyl aluminum (TNHA), or a sequential mixture of both activators. The catalyst precursor slurry was added to a mixing vessel at room temperature in an amount less than a stoichiometric amount, based on Lewis base present in the precursor. An appropriate amount of activator was added while stirring. If both activators were used, the DEAC solution was added first, and the slurry was stirred for one hour, followed by addition of the TNHA solution, followed by stirring for another two hours. If only DEAC or TNHA activator was used, addition was followed by stirring for at least one hour prior to use. Following partial activation, the slurry containing the partially activated precursor was retained at room temperature prior to use.


Representative Polymerization


For the inventive and comparative examples, ethylene was copolymerized with 1-hexene in two fluidized bed reactors. Each polymerization was continuously conducted after equilibrium was reached, under the respective conditions, as set forth in the respective tables of Tables 2A-6I, as shown below. Polymerization was initiated in the first reactor by continuously feeding the catalyst (Ziegler/Natta catalyst) and cocatalyst (trialkyl aluminum) into a fluidized bed of polyethylene granules, together with ethylene, 1-hexene and hydrogen. The resulting copolymer, mixed with active catalyst, was withdrawn from the first reactor and transferred to the second reactor, using second reactor gas as a transfer medium. The second reactor also contained a fluidized bed of polyethylene granules. Ethylene, 1-hexene, and hydrogen were introduced into the second reactor, where the gases come into contact with the polymer and catalyst from the first reactor. Inert gases, nitrogen and isopentane, make up the remaining pressure in both the first and second reactors. In the second reactor, the cocatalyst was again introduced. The final product blend was continuously removed. As known in the art, 1 kPa is 0.145 psi, 1 kg is 2.205 lb and 1 in is 25.4 mm.









TABLE 2A







INVENTIVE SAMPLES









SAMPLE NO.














I513
I514
I515
I516
I517
I922





Type
0017
0017
0017
0017
0017
Precursor



reduction
reduction
reduction
reduction
reduction



REACTION








CONDITIONS








(First Reactor)








Temp. ° C.
80.0
80.0
80.0
80.0
80.0
80.0


C2 Part. Pressure,
32.2
30.9
31.3
28.2
27.6
35.6


psi








H2/C2 Molar Ratio
0.034
0.034
0.034
0.034
0.035
0.034


C6/C2 Molar Ratio
0.070
0.070
0.062
0.080
0.081
0.087


Ethylene lb/hr
22.1
20.4
20.5
21.1
19.6
27.3


Hexene lb/hr
1.0
0.9
0.8
1.1
1.1
1.3


Hydrogen mlb/hr
6.3
5.8
6.0
5.6
5.1
6.4


Nitrogen lb/hr
6.1
6.2
6.1
6.0
5.8
4.5


Ethylene Mol %
10.3
9.9
10.0
9.0
8.8
11.4


Hexene Mol %
0.7
0.7
0.6
0.7
0.7
1.0


Hydrogen Mol %
0.3
0.3
0.3
0.3
0.3
0.4


Isopentane Mol %
7.8
6.5
6.7
8.0
6.7
8.0


Nitrogen Mol %
80.3
82.9
82.6
81.9
83.9
78.9


Cat cc/hr
2.2
2.2
2.2
2.2
2.2
14.4


E.B. Production
25.1
24.0
23.9
24.0
24.1
34.8


Rate, lb/hr








Bed Weight, lbs
68.8
69.6
69.6
70.4
70.4
68.5


FBD (lb/ft3)
21.5
22.4
22.6
22.7
23.2
11.8


Bed Volume, ft3
9.64
10.64
10.64
10.64
10.64
11.64


Residence Time, hr
2.7
2.9
2.9
2.9
2.9
2.0


STY, lb/hr/ft3
2.6
2.3
2.3
2.3
2.3
3.0


SGV (ft/sec)
2.6
3.6
4.6
5.6
6.6
11.6
















TABLE 2B







INVENTIVE SAMPLES continued









SAMPLE NO.














I513
I514
I515
I516
I517
I922
















RESIN








PROPERTIES








(First Reactor)








Flow Index,
0.59
0.56
0.50
0.62
0.57
0.55


dg/min I21








Melt Index,








dg/min I2








Density, g/cm3
0.9250
0.9246
0.9257
0.9235
0.9232
0.9231


MFR








Titanium,
1.9
2.0
2.1
1.9
2.0
1.8


ppmw








Aluminum
87.5
93.2
97.7
93.9
94.9
70.1


ppmw








Al/Ti
83.7
81.3
81.3
87.9
84.8
70.9


Bulk Density,
17.7
17.5
17.4
17.0
17.1
15.5


lb/ft3








APS, inches
0.032
0.030
0.029
0.031
0.028
0.038


Fines, Wt % LT
1.5
1.3
1.5
1.6
2.8
0.7


120 Mesh








GPC Analysis








Conventional








Mn
73300.0
70700.0
71100.0
66200.0
65500.0



Mw
323000.0
320000.0
315000.0
306000.0
270000.0



Mw/Mn
4.41
4.53
4.43
4.62
4.12



Mz
911000.0
930000.0
849000.0
842000.0
711000.0



Absolute








Mn
83100.0
81300.0
84400.0
76400.0
75800.0



Mw
367000.0
361000.0
360000.0
350000.0
310000.0



Mz
1031000.0
1008000.0
1000000.0
1000000.0
854000.0



Mz/Mw
2.81
2.79
2.78
2.86
2.75



g′
1.03
1.03
1.03
1.03
1.03
















TABLE 2C







INVENTIVE SAMPLES continued









SAMPLE NO.














I513
I514
I515
I516
I517
I922
















REACTION








CONDITIONS








(Second








Reactor)








Temp. ° C.
95.0
95.0
95.0
94.9
95.0
94.9


Pressure, psig
397.1
397.1
397.0
396.8
397.1
342.1


C2 Part.
95.2
94.0
92.7
101.8
85.5
108.8


Pressure, psi








H2/C2 Molar
0.4
0.7
0.5
0.3
0.9
0.5


Ratio








C6/C2 Molar
0.03
0.03
0.03
0.03
0.03
0.03


Ratio








Ethylene lb/hr
31.1
26.4
27.0
37.8
14.4
36.6


Hexene lb/hr
0.9
0.9
0.8
0.8
0.5
1.1


Isopentane
0.3
0.0
0.0
0.0
0.7
1.0


lb/hr








Nitrogen lb/hr
20.5
15.4
17.4
21.6
14.3
14.5


Ethylene Mol
23.1
22.8
22.5
24.7
20.7
30.5


%








Hexene Mol %
0.7
0.7
0.7
0.7
0.5
1.0


Hydrogen Mol
9.0
15.6
10.9
7.4
18.0
15.3


%








Isopentane
1.0
0.8
0.8
1.0
1.0
0.3


Mol %








Nitrogen Mol
63.9
59.1
63.7
64.1
58.8
52.2


%








E.B.
17.9
14.7
17.2
21.3
13.6
24.4


Production








Rate, lb/hr








Bed Weight,
107.4
107.9
107.3
107.6
107.1
100.1


lbs








Fluidized Bed
13.4
13.5
13.5
12.8
13.4
13.4


Density (lb/ft3)








Bed Volume,
11.0
12.0
12.0
12.0
12.0
13.0


ft3








Residence
2.50
2.79
2.61
2.38
2.84
1.69


Time, hr








Space Time
3.9
3.2
3.4
3.8
3.1
4.6


Yield, lb/hr/ft3








Superficial gas
1.7
1.6
1.7
1.7
1.6
1.7


velocity (ft/sec)
















TABLE 2D







INVENTIVE SAMPLES continued









SAMPLE NO.














I513
I514
I515
I516
I517
I922
















RESIN PROPERTIES (Blend)








Flow Index, dg/min I21 (G)
8.1
9.0
8.4
8.4
10.1
9.4


Melt Index, dg/min I2 (G)
0.16
0.15
0.14
0.18
0.15
0.17


Density, g/cm3 (G)
0.9394
0.9406
0.9407
0.9390
0.9406
0.9392


MFR (MI21/MI2) (G)
51.3
59.3
57.8
46.0
68.3
56.0


Titanium, ppmw (G)
1.0
1.6
1.1
1.0
1.2
0.9


Aluminum ppmw (G)
60.7
66.1
65.1
56.3
72.2
45.6


Al/Ti (G)
112.4
75.1
105.1
98.5
106.8
89.1


Bulk Density, lb/ft3 (G)
20.2
20.6
20.1
19.6
20.6
18.0


APS, inches (G)
0.030
0.027
0.027
0.030
0.028
0.035


Fines, Wt % less than120 Mesh (G)
2.2
2.9
2.0
2.2
3.5
1.3


Split % by Energy Balance (G)
58.3
61.9
58.2
53.0
63.9
58.8


Split % Calculated (G) [Split % =
48.5
53.3
49.2
43.0
54.4
48.5


weight of HMW/(sum weight (HMW +








LMW)) × 100]








MI2 - g/10 min (P)
0.16
0.17
0.16
0.18
0.14
0.19


ASTM D-1238-04








MI5 - g/10 min (P)
0.54
0.63
0.54
0.65
0.55
0.70


ASTM D-1238-04








MI10 - g/10 min (P)
1.80
2.26
1.88
2.07
1.96
2.34


ASTM D-1238-04








MI21 - g/10 min (P)
7.75
11.10
8.85
8.88
10.33
11.34


ASTM D-1238-04








MFR (I21/I2) (P)
49.9
67.2
56.6
48.4
72.9
59.8


ASTM D-1238-04








MFR (I21/I5) (P)
14.2
17.6
16.4
13.7
18.8
16.2


ASTM D-1238-04








MFR (I10/I2) (P)
11.6
13.7
12.0
11.3
13.8
12.3


ASTM D-1238-04








Density (g/cc) (P)
0.9445
0.9464
0.946
0.9447
0.9457
0.945


ASTM D-792-00








IR structure (P)








Trans/1000 carbons (P)
0.02
0
0.013
0.015
0.0012
0.024


ASTM D6248-2004








Vinyls/1000 carbons (P)
0.21
0.25
0.22
0.2
0.22
0.18


ASTM D6248-2004








Methyls/1000 carbons (P)
3
3.4
2.8
3.1
4.1
3.5


ASTM D2238-1999





G = Granular Polymer


P = Pelletized Polymer with Additives and Pigments


[Split % (calculated) = (weight of HMW/(sum weight (HMW + LMW))) × 100]













TABLE 2E







INVENTIVE SAMPLES continued









SAMPLE NO.













Additive analysis
I513
I514
I515
I516
I517
I922
















Irganox 1010 ppm
1372
1378
1309
1396
1484
1409


Irgafos 168 ppm total
1601
1523
1544
1608
1596
785


Irgafos 168 ppm
1108
1350
1196
1064
1339
815


Active








Irgafos 168 ppm
492
173
348
544
257
1600


Inactive








Percent Active I-168
69.3
88.6
77.5
66.2
83.9
49.1


RMS-100 Viscosity
83172
81192
90984
68549
91009
784000


MPa at 0.01 sec−1








shear rate








RMS-800 Viscosity
2653
2267
2547
2659
2296
24093


MPa at 100 sec−1








shear rate








G′/G″ @ 0.01 sec−1
0.289
0.298
0.309
0.268
0.308
0.324


Shear Rate








G′/G″ @ 0.1 sec−1
0.418
0.432
0.443
0.387
0.448
0.438


Shear Rate








Viscosity ratio
31.4
35.8
35.7
25.8
39.6
32.5


0.01/100 data








Rheotens melt
10.5
9.1
10.5
9.5
10.5
9.5


strength (cN)








Rheotens Velocity
125
125
145
140
125
145


(mm)








DSC Melting Point
128.54
128.84
128.74
128.6
128.28
129.27


(Deg C.)








ASTM D-3418-03








Heat of Fusion (J/g)
187.2
192.1
189.5
187
190.2
177.3


ASTM D-3418-03








DSC Crystallization
117.08
117.03
117.34
117.09
116.91
115


point (Deg C.)








ASTM D-3418-03








Heat of Crystallization
184.1
191.3
188.8
187.1
192.1
172.4


(J/g)








ASTM D-3418-03








DSC Induction Time
69.16
50.81
84.24
~40
85.46



(min)








ASTM D-3350-05








DSC Induction Temp
244.8
238.9
238.8
243.4
249.5



(Deg C.)








ASTM D-3350-05








C13 NMR Wt %
2.3
2.2
2
2.2
2.5
2.5


Hexene








ASTM D-5017-91








Branches/1000 C. in
3.7
3.6
3.3
3.3
3.8



Backbone








ASTM D-5017-91








Atref HD fraction (%)
75.2
76.3
78.2
80.9
72.5
77


Temperature
86
86
86.1
86.1
86.1
86


Minimum (C.)








SCB portion
13.9
11.6
9.7
10.3
15.6
11


SCB portion
52
52
58
62
51
60


minimum temperature








(C.)








SCB distribution Mv
93249
92200
97395
98596
80000
90569


ATREF Purge (%)
10.9
12.1
12.1
8.8
11.9
12.0
















TABLE 2F







INVENTIVE SAMPLES continued









SAMPLE NO.














I513
I514
I515
I516
I517
I922
















Purge Mv
59223
52362
57004
39936
44738
74334


ATREF Overall
89540
87380
92508
93434
75803
88621


Mv Average








ATREF Dv
−0.0041
−0.015
−0.019
−0.015
−0.0093
−0.013


viscosity -








temperature








slope (70-90 C.








region)








Triple Detector








Results








Conventional








GPC








Mn
30920
24880
28400
36700
24310
27380


Mw
201830
198560
198610
194360
199440
128890


Mz
801400
839800
800000
770200
804700
426900


Mw/Mn
6.5
8.0
7.0
5.3
8.2
4.7


Absolute GPC








Mn
29684
24615
28616
35350
23440
27980


Mw
219050
210860
214870
208740
211090
158820


Mw (abs)/Mn
7.4
8.6
7.5
5.9
9.0
5.7


abs








Mz (BB)
815800
830100
813700
775900
854300
570600


Mz (abs)
898400
902100
886800
906300
953400
969800


Mz + 1 (BB)
1467700
1459100
1453200
1407700
1486600
1164800


Mz (abs)/Mw
4.1
4.3
4.1
4.3
4.5
6.1
















TABLE 2G







INVENTIVE SAMPLES continued









SAMPLE NO.














I513
I514
I515
I516
I517
I922
















Plaque Properties








PENT (2.4 MPa) Hrs
>9,300  
>10,000  
>10,000  
>10,000  
>10,000  
>15,000


ASTM D-1473-01





(on test)


RCP Gc @ 23 C. from
Incomplete
178 and
Incomplete
Incomplete
221 and
196


PENT plaque milled
break no
Incomplete
break no
break no
Incomplete



to 2 mm thick samples
reading
break
reading
reading
break



(KJ/m2)
available

available
available




Modified (2 mm)








ASTM F-2231-02








RCP Gc @ 23 C. from
 189
  109.8
 156
 169
 116



PENT plaque milled








to 3 mm thick samples








(KJ/m2)








ASTM F-2231-02








Flexural Modulus
136500 
151400 
144600 
137000 
138500 
139200


(psi) @ 0.5 inches/min








ASTM D-790-03








SD
10400 
4536
6700
9314
8660
8820


Secant Modulus (psi)
91300 
98800 
96800 
92000 
95200 
98100


2% @ 0.5 inches/min








ASTM D-790-03








SD
2300
2178
2100
1624
1920
2162


Secant Modulus (psi)
109600 
119400 
116400 
110200 
114200 
117400


1% @ 0.5 inches/min








ASTM D-790-03








SD
3440
2897
3000
2693
2500
3100


Tensile Strength (PSI)
5327
5070
5280
5565
5168
4920


ASTM D-638-03








SD
 230
 475
 317
 228
 204
542


% Elongation
 730
 730
 730
 731
 693
698


ASTM D-638-03








SD
 13
 25
 20
   12.6
 15
35


Yield Strength (psi)
2460
2590
2570
2593
2700
2537


ASTM D-638-03








SD
 53
 ~40
 58
 197
 268
38


Yield Strain (%)
   4.1
  4
   3.8
    4.97
   5.8
4.85


ASTM D-638-03








SD
    0.17
   0.1
   0.1
    1.84
   2.8
0.28


Burst Properties








10**5 intercept at 23 C.
>1347 
>1333 
>1358 
>1334 
>1366 
1338


(psi)








ASTM D-1598-02








ASTM D-2837-04








10**5 intercept at 60 C.,
 >961*
 >966*
 >963*
 >978*
 >969*
983


(psi)








ASTM D-1598-02








ASTM D-2837-04








Hours on test at 60 C.
>12000* 
>12000* 
>12000* 
>12000* 
>12000* 
>14084


90 C. validation test
in progress
In progress
In progress
passed
in progress
Pass


(690 psi Hoop stress








for >3800 hours)








PPI TR #3 Section








F.4.2.1





*Still on test.













TABLE 3A







COMPARATIVE SAMPLES









SAMPLE NO.













C024
C025
C453
C454
C510





Type
precursor
precursor
precursor
precursor
0017







reduction


First Reactor







REACTION CONDITIONS







Temp. ° C.
80
80
80
80
80


C2 Part. Pressure, psi
25
24
27
27
34.0


H2/C2 Molar Ratio
0.027
0.015
0.023
0.022
0.030


C6/C2 Molar Ratio
0.08
0.125
0.105
0.125
0.087


Ethylene lb/hr
21.3
22.4
23
24.3
20.7


Hexene lb/hr
1.2
2.2
2
2.4
1.3


Hydrogen mlb/hr




5.9


Isopentane lb/hr
0
0
2
2
0.0


Nitrogen lb/hr




5.9


Ethylene Mol %




10.8


Hexene Mol %




0.9


Hydrogen Mol %




0.3


Isopentane Mol %




7.5


Nitrogen Mol %




80.8


Cat cc/hr




2.2


E.B. Production Rate, lb/hr
26
28
28
30
25.0


Bed Weight, lbs




63.3


FBD (lb/ft3)




21.3


Bed Volume, ft3




8.64


Residence Time, hr
3.88
3.47
3.66
2.88
2.5


STY, lb/hr/ft3
2.6
2.9
2.2
3.3
2.9


SGV (ft/sec)




1.6
















TABLE 3B







COMPARATIVE SAMPLES









SAMPLE NO.













C024
C025
C453
C454
C510















RESIN







PROPERTIES (First







reactor)







Flow Index, dg/min
0.44
0.45
0.43
0.44
0.63


I21







Melt Index, dg/min







I2







Density, g/cm3
0.9238
0.9166
0.9187
0.9162
0.9230


MFR







Titanium, ppmw
2.73
2.28
2.21
2.43
1.7


Aluminum ppmw
76.5
68.3
99.7
90.9
82.7


Al/Ti




85.5


Bulk Density, lb/ft3
18.8
17.9
18.1
17.5
15.0


APS, inches
0.0272
0.0316
0.031
0.0289
0.033


Fines, Wt % LT 120
2.7
1.9
2.1
2.3
0.5


Mesh







GPC Analysis







Conventional







Mn




66400.0


Mw




262300.0


Mw/Mn




3.95


Mz




714000.0


Absolute







Mn




88900.0


Mw




316000.0


Mz




936000.0


Mz/Mw




2.96


g′




1.03


Weight Fraction




0.957


<1,000,000
















TABLE 3C







COMPARATIVE SAMPLES









SAMPLE NO.













C024
C025
C453
C454
C510















REACTION







CONDITIONS







(Second reactor)







Temp. ° C.
100
100
100
100
95.0


Pressure, psig
397
398
373
393
397.1


C2 Part. Pressure,
79
86.4
82.5
92.3
104.6


psi







H2/C2 Molar Ratio
1.75
1.75
1.75
1.75
0.5


C6/C2 Molar Ratio
0.053
0.025
0.015
0.025
0.02


Ethylene lb/hr
21.8
24.6
18.8
27.9
25.9


Hexene lb/hr
1.3
0.6
0.4
0.9
0.7


Isopentane lb/hr




0.5


Nitrogen lb/hr




14.6


Ethylene Mol %




25.4


Hexene Mol %




0.6


Hydrogen Mol %




12.7


Isopentane Mol %




1.0


Nitrogen Mol %




59.5


E.B. Production
19.5
21
16.6
22.5
17.0


Rate, lb/hr







Bed Weight, lbs
132.4
133.7
116.9
117.5
108.3


Fluidized Bed




12.4


Density (lb/ft3)







Bed Volume, ft3




10.0


Residence Time, hr
5.99
5.36
4.88
3.86
2.58


Space Time Yield,
2.2
2.5
1.9
2.9
4.2


lb/hr/ft3







Superficial gas




1.7


velocity (ft/sec)
















TABLE 3D







COMPARATIVE SAMPLES








RESIN



PROPERTIES
SAMPLE NO.












(Blend)
C024
C025
C453
C454
C510















Flow Index, dg/min I21 (G)
13.2
14.3
9.5
20.9
9.6


Melt Index, dg/min
0.14
0.13
0.09
0.16
0.16


I2 (G)







Density, g/cm3 (G)
0.9414
0.9395
0.9397
0.9403
0.9396


MFR (MI21/MI2)
97.7
111.1
103.9
132.8
58.9


(G)







Titanium, ppmw (G)
1.49
1.3
1.36
1.29
1.0


Aluminum ppmw
55.3
47
71.3
52.1
62.4


(G)







Al/Ti (G)




114.4


Bulk Density, lb/ft3
23
22.4
21.8
21.6
18.1


(G)







APS, inches
0.0271
0.0303
0.031
0.029
0.030


Fines, Wt % less
3.3
3
2.7
3
1.4


than120 Mesh (G)







Split % by Energy
57.2
57.2
62.7
57.2
59.6


Balance







Split % calculated
54.0
53.3
57.4
49.0
49.5


(G)





[Split % (calculated) = weight of HMW/(sum weight (HMW + LMW)) × 100]













TABLE 3E







COMPARATIVE SAMPLES









SAMPLE NO.













C024
C025
C453
C454
C510















MI2 - g/10 min
0.14
0.12
0.09
0.17
0.19


(P)







ASTM D-1238-







04







MI5 - g/10 min
0.48
0.61
0.39
0.66
0.69


(P)







ASTM D-1238-







04







MI10 - g/10 min
1.95
3.47
1.47
3.26
2.31


(P)







ASTM D-1238-







04







MI21 - g/10 min
27.4
15.1
10.16
19.9
10.77


(P)







ASTM D-1238-







04







MFR (I21/I2)
195.7
125.8
112.9
117.1
56.5


(P)







MFR (I21/I5)
57.1
24.8
26.1
30.2
15.6


(P)







MFR (I10/I2)
13.9
28.9
16.3
19.2
12.1


(P)







Density (g/cc)
0.942
0.9406
0.9406
0.9406
0.9448


(P)ASTM D-







792-00







IR structure (P)







Trans/1000
0.005
0.008
0.005
0.012
0.016


carbons (P)







ASTM D-6248-







2004







Vinyls/1000
0.099
0.167
0.128
0.192
0.22


carbons (P)







ASTM D-6248-







2004







Methyls/1000
5.1
6.23
5.21
5.22
3.7


carbons (P)







ASTM D-2238-







1999
















TABLE 3F







COMPARATIVE SAMPLES









SAMPLE NO.












Additive analysis
C024
C025
C453
C454
C510















Irganox 1010 ppm


1708
1866
1422


Irgafos 168 ppm total


1580
1838
1549


Irgafos 168 ppm Active


1459
1664
1178


Irgafos 168 ppm Inactive




371


Percent Active I-168


0.92
0.91
76.0


RMS-100 Viscosity MPa at




72407


0.01 sec−1 shear rate







RMS-800 Viscosity MPa at




2360


100 sec−1 shear rate







G′/G″ @ 0.01 sec−1 Shear




0.279


Rate







G′/G″ @ 0.1 sec−1 Shear




0.41


Rate







Viscosity ratio 0.01/100




30.7


data







Rheotens melt strength (cN)




9.3


Rheotens Velocity (mm)




135


DSC Melting Point




128.83


(Deg C.)







ASTM D-3418-03







Heat of Fusion (J/g)




189.4


ASTM D-3418-03







DSC Crystallization point




117.05


(Deg C.)







ASTM D-3418-03







Heat of Crystallization (J/g)




188.2


ASTM D-3418-03







DSC Induction Time (min)




>90


ASTM D-3350-05







DSC Induction Temp (Deg




247.5


C.)







ASTM D-3350-05
















TABLE 3G







COMPARATIVE SAMPLE









SAMPLE NO.













C024
C025
C453
C454
C510
















C13 NMR Wt %




2.4


Hexene


ASTM D-5017-


91


Branches/1000 C.




3.9


in Backbone


ASTM D-5017-


91


Atref HD fraction


59.2
59
76.2


(%)


Temperature


86
86.2
86.1


Minimum (C.)


SCB portion


23.8
22
13.3


SCB portion


52
54
50


minimum


temperature (C.)


SCB distribution


92376
90910
98920


Mv


Aterf Purge (%)


23.3
19
10.5


Purge Mv


140531
109153
76650


Atref Overall Mv


103596
94376
96582


Average


Atref Dv


0.0041
0.0011
−0.0023


viscosity -


temperature


slope


(70-90 C. region)


Triple Detector


Results


Conventional


GPC


Mn




26580


Mw




195000


Mz




829200


Mw/Mn




7.3


Absolute GPC


Mn




27433


Mw




212800


Mw (abs)/Mn




7.8


Abs


Mz(BB)




833100


Mz (abs)




921700


Mz + 1 (BB)




1490000


Mz (abs)/Mw




4.3
















TABLE 3H







COMPARATIVE SAMPLE









SAMPLE NO.













C024
C025
C453
C454
C510
















Plague Properties







PENT (2.4 MPa)
>4463
>5498
>4844
>8909
>8549


Hrs

@2.6
@2.6
@2.6


ASTM D-1473-01


RCP Gc @ 23 C.
165
222
225
214
Incomplete


from PENT plaque




break no


milled to 2 mm




reading


thick samples




available


(KJ/m2)


Modified (2 mm)


ASTM F-2231-02


RCP Gc @ 23 C.




214


from PENT plaque


milled to 3 mm


thick samples


(KJ/m2)


ASTM F-2231-02


Flexural Modulus
148000
140000
151000
150000
136600


(psi) @ 0.5 inches/min


ASTM


D-790-03


SD




7438


Secant Modulus
100700
96700
100000
97000
94900


(psi) 2% @ 0.5 inches/min


ASTM D-790-03


SD




2515


Secant Modulus
120000
115000
120000
117000
112700


(psi) 1% @ 0.5 inches/min


ASTM D-790-03


SD




3762


Tensile Strength
4740
4680
4214
4335
5071


(PSI)


ASTM D-638-03


SD




441


% Elongation
720
675
730
710
710


ASTM D-638-03


SD




17.4


Yield Strength (psi)
3014
2849
2744
2718
2521


ASTM D-638-03


SD




141


Yield Strain (%)
5.4
6.4
7.4
7.1
5.97


ASTM D-638-03


SD




4.4
















TABLE 3I







COMPARATIVE SAMPLE









SAMPLE NO.













C024
C025
C453
C454
C510
















Burst Properties







10**5 intercept at
NA
NA
NA
NA
Failed


23 C. (psi)




Screening


ASTM D-1598-02




test @ 60 C.


ASTM D-2837-04


10**5 intercept at
Failed
Failed
Failed
Failed
Failed


60 C., (psi)




Screening


ASTM D-1598-02




test


ASTM D-2837-04


90 C. validation test
NA
NA
NA
NA
NA


(690 psi Hoop stress


for >3800 hours)





NA = Not Applicable













TABLE 4A







COMPARATIVE SAMPLES









SAMPLE NO.














C512
C586
C587
C588
C589
C590

















Type
0017
0017
0017
0017
0017
0017



reduction
reduction
reduction
reduction
reduction
reduction


First Reactor


REACTION


CONDITIONS


Temp. ° C.
80.0
80.0
80.0
80.0
80.0
80.0


C2 Part. Pressure,
30.7
25.8
24.4
23.9
26.9
36.1


psi


H2/C2 Molar Ratio
0.026
0.050
0.053
0.037
0.062
0.043


C6/C2 Molar Ratio
0.092
0.047
0.076
0.042
0.040
0.025


Ethylene lb/hr
21.9
21.3
22.8
21.7
22.3
21.7


Hexene lb/hr
1.3
0.7
1.2
0.6
0.6
0.5


Hydrogen mlb/hr
5.1


Isopentane lb/hr

3.0
3.0
3.0
3.0
3.0


Nitrogen lb/hr
6.0


Ethylene Mol %
9.8


Hexene Mol %
0.9


Hydrogen Mol %
0.3


Isopentane Mol %
7.3


Nitrogen Mol %
82.1


Cat cc/hr
2.2


E.B. Production
25.0
26.0
26.9
26.1
25.9
26.0


Rate, lb/hr


Bed Weight, lbs
70.2


FBD (lb/ft3)
22.5


Bed Volume, ft3
9.64


Residence Time, hr
2.8
2.9
2.8
2.9
2.9
2.8


STY, lb/hr/ft3
2.6
1.8
2.7
2.4
2.4
2.4


SGV (ft/sec)
2.6
















TABLE 4B







COMPARATIVE SAMPLES









SAMPLE NO.














C512
C586
C587
C588
C589
C590

















RESIN








PROPERTIES


(First reactor)


Flow Index,
0.54
0.5
0.61
0.3
0.60
0.27


dg/min I21


Melt Index, dg/min








I2


Density, g/cm3
0.9212
0.9291
0.9248
0.9284
0.9306
0.9300


MFR








Titanium, ppmw
1.9
3.8
3.3
4.5
3.8
4.2


Aluminum ppmw
89.0
110.0
80.7
113.4
113.4
97.8


Al/Ti
85.2
51.6
44.5
45.2
53.9
41.3


Bulk Density,
17.0
20.4
20.8
21.4
22.2
24.8


lb/ft3


APS, inches
0.033
0.028
0.027
0.028
0.027
0.025


Fines, Wt % LT
1.1
1.1
1.4
1.1
1.3
0.9


120 Mesh


GPC Analysis


Conventional


Mn
65900.0


Mw
259000.0


Mw/Mn
3.93


Mz
659000.0


Absolute


Mn
77600.0


Mw
293000.0


Mz
771000.0


Mz/Mw
2.63


g′
1.03


Weight Fraction
0.962


<1,000,000
















TABLE 4C







COMPARATIVE SAMPLES









SAMPLE NO.














C512
C586
C587
C588
C589
C590

















REACTION








CONDITIONS


(Second reactor)


Temp. ° C.
95.0
94.9
94.9
95.3
99.9
94.9


Pressure, psig
397.3
392.6
392.6
392.5
392.8
393.0


C2 Part. Pressure, psi
102.9
63.0
68.8
65.5
61.6
76.9


H2/C2 Molar Ratio
0.6
1.3
1.3
1.3
1.8
1.3


C6/C2 Molar Ratio
0.02
0.07
0.03
0.08
0.08
0.08


Ethylene lb/hr
30.3
16.4
20.8
19.9
18.2
21.3


Hexene lb/hr
0.5
1.2
0.8
1.5
1.5
1.6


Isopentane lb/hr



Nitrogen lb/hr
22.1


Ethylene Mol %
24.9


Hexene Mol %
0.6


Hydrogen Mol %
15.1


Isopentane Mol %
1.0


Nitrogen Mol %
57.4


E.B. Production Rate, lb/hr
16.6
15.6
16.9
18.0
15.7
19.0


Bed Weight, lbs
107.3
91.1
89.1
91.0
90.3
89.4


Fluidized Bed
13.5


Density (lb/ft3)


Bed Volume, ft3
11.0


Residence Time, hr
2.58
2.2
2.0
2.1
2.2
2.0


Space Time Yield,
3.8
2.7
3.9
3.7
3.5
3.8


lb/hr/ft3


Superficial gas
1.6


velocity (ft/sec)
















TABLE 4D







COMPARATIVE SAMPLES









SAMPLE NO.














C512
C586
C587
C588
C589
C590

















RESIN








PROPERTIES


(Blend)


Flow Index,
9.9
8.9
10.0
8.1
9.8
8.0


dg/min I21 (G)


Melt Index, dg/min I2 (G)
0.15
0.12
0.14
0.09
0.13
0.10


Density, g/cm3
0.9395
0.9407
0.9407
0.9401
0.9408
0.9408


(G)


MFR (MI21/MI2)
65.0
71.5
70.7
90.6
75.5
83.0


(G)


Titanium, ppmw
1.0
2.2
2.0
2.4
2.3
2.3


(G)


Aluminum ppmw
60.0
71.2
56.7
66.6
69.6
49.0


(G)


Al/Ti (G)
106.0
58.1
49.9
49.8
53.6
37.4


Bulk Density,
20.0
23.6
23.7
24.2
24.3
27.2


lb/ft3 (G)


APS, inches (G)
0.031
0.027
0.026
0.0
0.026
0.027


Fines, Wt % less
2.3
3.0
2.8
2.6
1.9
1.0


than120 Mesh (G)


Split % by Energy
60.1
62.5
61.4
59.2
62.2
57.7


Balance(G)


Split % calculated
49.8
57.3
57.7
53.7
60.6
52.9


(G)





[Split % (calculated) = (weight of HMW/(sum weight (HMW + LMW))) × 100]













TABLE 4E







COMPARATIVE EXAMPLES









SAMPLE NO.














C512
C586
C587
C588
C589
C590

















MI2 - g/10 min (P)
0.15
0.12
0.14
0.08
0.13
0.1


ASTM D-1238-04


MI5 - g/10 min (P)
0.59
0.47
0.53
0.34
0.47
0.38


ASTM D-1238-04


ASTM D-1238-04
1.97
1.6
1.8
1.3
1.7
1.4


MI21 - g/10 min(P)
10.21
8.6
9.4
7.6
9.5
8.1


ASTM D-1238-04


MFR (I21/I2) (P)
68.4
71.7
67.1
95.0
73.1
81.0


MFR (I21/I5) (P)
17.2
18.3
17.7
22.4
20.2
21.3


MFR (I10/I2) (P)
13.2
13.3
12.9
16.3
13.1
14.0


Density (g/cc) (P)
0.9451
0.9413
0.9408
0.9407
0.9412
0.9419


ASTM D-790-00


IR structure (P)


Trans/1000
0.009
0.012
0.008
0.01
0
0.01


carbons (P)


ASTM D-6248-


2004


Vinyls/1000
0.23
0.148
0.135
0.167
0.14
0.148


carbons (P)


ASTM D-6248-


2004


Methyls/1000
4.1
3.2
3.17
3.99
4.2
3.72


carbons (P)


ASTM D-2238-


1999


Additive analysis


Irganox 1010 ppm
1458
1392
1278
1645
1246
1359


Irgafos 168 ppm
1573
1365
1310
1662
1216
1393


total


Irgafos 168 ppm
1276
1153
1129
1472
1019
1215


Active


Irgafos 168 ppm
297
212
181
190
197
178


Inactive


Percent Active I-
81.1
0.84
0.86
0.89
0.84
0.87


168
















TABLE 4F







COMPARATIVE EXAMPLES









SAMPLE NO.














C512
C586
C587
C588
C589
C590

















RMS-100
90795
1.10E+05
9.80E+04
1.60E+05
1.10E+05
1.30E+05


Viscosity MPa at


0.01 sec−1 shear


rate


RMS-800
2370
2460
2460
2550
2410
2560


Viscosity MPa at


100 sec−1 shear


rate


G′/G″ @ 0.01 sec−1
0.305
0.33
0.29
0.37
0.32
0.33


Shear Rate


G′/G″ @ 0.1 sec−1
0.451
0.47
0.43
0.54
0.46
0.48


Shear Rate


Viscosity ratio
38.3
44.7
39.8
62.7
45.6
50.8


0.01/100 data


Rheotens melt
10.5


strength (cN)


Rheotens Velocity
145


(mm)


DSC Melting Point
128.67
128.31
128.05
128.88
128.89
129.01


(Deg C.)


ASTM D-3418-03


Heat of Fusion
189.3
181.5
179
179.4
181
179.6


(J/g)


ASTM D-3418-03


DSC
117.04
116.09
116.03
115.65
115.56
116.11


Crystallization


and 76.38


point (Deg C.)


ASTM D-3418-03


Heat of
188.4
176.1
178.9
178.7
176.7
177.6


Crystallization


(J/g)


ASTM D-3418-03


DSC Induction
60.07
32.29
40.73
54.74
34.53
55.94


Time (min)


ASTM D-3350-05


DSC Induction
237.9
235.25
242.28
244.83
237.65
244.61


Temp (Deg C.)


ASTM D-3350-05
















TABLE 4G







COMPARATIVE EXAMPLES









SAMPLE NO.














C512
C586
C587
C588
C589
C590

















C13 NMR Wt %
2.5
2.8
3
2.9
3.1
3


Hexene


ASTM D-5017-91


Branches/1000 C. in
4.2


Backbone


ASTM D-5017-91


Atref HD fraction
73.8
68.8
72.8
68.2
66.1
71.5


(%)


Temperature
86.1
86
86.1
86
86
86.1


Minimum (C.)


SCB portion
14.3
16.2
13.8
18
19.6
16.9


SCB portion
50
50
55
37
45
45


minimum


temperature (C.)


SCB distribution Mv
78786


Aterf Purge (%)
11.9
15
13.4
13.8
14.3
11.6


Purge Mv
52026
110086
106484
116470
102464
92141


Atref Overall Mv
75602
117608
106552
125155
116623
115821


Average


Atref Dv viscosity -
0.0024
0.021
0.0028
0.019
0.069
0.069


temperature slope


(70-90 C. region)


Triple Detector


Results


Conventional GPC


Mn
27620
15950
20120
16670
11740
13120


Mw
199810
196180
201500
209430
198450
207000


Mz
816600
835700
876700
878600
869700
886800


Mw/Mn
7.2
12.3
10.0
12.6
16.9
15.8


Absolute GPC


Mn
26385
18821
23840
20437
14325
15633


Mw
210240
226160
227130
243880
244730
219720


Mw (abs)/Mn abs
8.0
12.0
9.5
11.9
17.1
14.1


Mz(BB)
861700
914200
912500
991700
926800
945000


Mz (abs)
924800
1075400
1070100
1134800
1172500
987500


Mz + 1 (BB)
1539000
1764000
1808700
1850200
1725700
1799900


Mz (abs)/Mw
4.4
4.76
4.71
4.65
4.79
4.49


Mw (abs)/Mw

1.15
1.13
1.16
1.23
1.06


(GPC)
















TABLE 4H







COMPARATIVE SAMPLES









SAMPLE NO.














C512
C586
C587
C588
C589
C590

















Plaque Properties








PENT (2.4 MPa)
>8279
>19442
>19685
>19594
7923
2095


Hrs

(discont'd)
(discont'd)
(discont'd)


ASTM D-1473-01


RCP Gc @ 23 C.
Incomplete
134
155
118
57
121


from PENT plaque
break no


milled to 2 mm thick
reading


samples (KJ/m2)
available


Modified (2 mm)


ASTM F-2231-02


RCP Gc @ 23 C.
176


from PENT plaque


milled to 3 mm thick


samples (KJ/m2)


ASTM F-2231-02


Flexural Modulus
135800
137000
135000
131000
138000
136000


(psi) @ 0.5 inches/min


ASTM D-790-03


SD
5944


Secant Modulus
96200
97400
100000
92500
97600
97500


(psi) 2% @ 0.5 inches/min


ASTM D-790-03


SD
2550


Secant Modulus
114200
117000
119000
111000
117000
118000


(psi) 1% @ 0.5 inches/min


ASTM D-790-03


SD
3670


Tensile Strength
5088
5320
5370
5250
5190
5060


(PSI)


ASTM D638-03


SD
412


% Elongation
710
880
780
870
961
960


ASTM D638-03


SD
14


Yield Strength (psi)
2483
2900
2790
2750
2940
3030


ASTM D638-03


SD
77


Yield Strain (%)
3.974
7.7
6.5
7.4
7.5
6.1


ASTM D638-03


SD
0.09
















TABLE 4I







COMPARATIVE EXAMPLES









SAMPLE NO.














C512
C586
C587
C588
C589
C590

















Burst Properties








10**5 intercept at 23 C.
Failed
NA
NA
NA
NA
NA


(psi)
Screening


ASTM D-1598-02
test @ 60 C.


ASTM D-2837-04


10**5 intercept at
Failed
Failed
Failed
Failed
Failed
Failed


60 C., (psi)
Screening


ASTM D-1598-02
test


ASTM D-2837-04


90 C. validation
NA
NA
NA
NA
NA
NA


test (690 psi Hoop


stress for >3800 hours)


PPI TR #3 Section


F.4.2.1





NA = Not Applicable













TABLE 5A







COMPARATIVE SAMPLES









SAMPLE NO.













C591
C592
C636
C916
C918
















Type
0017
0017
Precursor
Precursor
Precursor



reduction
reduction


Temp. ° C.
80.0
80.0
80
80.0
80.0


C2 Part. Pressure, psi
31.9
29.1
28
32.0
33.4


H2/C2 Molar Ratio
0.061
0.043
0.02930
0.037
0.037


C6/C2 Molar Ratio
0.038
0.067
0.0617
0.084
0.084


Ethylene lb/hr
21.7
22.7

26.7
27.1


Hexene lb/hr
0.6
1.2

1.3
1.3


Hydrogen mlb/hr



2.5
2.2


Isopentane lb/hr
3.0
3.0





Nitrogen lb/hr



4.4
4.2


Ethylene Mol %



10.2
10.6


Hexene Mol %



0.9
0.9


Hydrogen Mol %



0.4
0.4


Isopentane Mol %



8.0
8.0


Nitrogen Mol %



80.2
80.0


Cat cc/hr


2.7
4.4
13.4


E.B. Production
26.0
27.3
24.0
34.8
35.1


Rate, lb/hr


Bed Weight, lbs


98.4
68.3
68.5


FBD(lb/ft3)


12.0
13.2
12.8


Bed Volume, ft3


8.2
8.64
10.64


Residence Time, hr
2.8
2.7
4.10
2.0
1.9


STY, lb/hr/ft3
2.4
2.8
2.9
4.0
3.3


SGV (ft/sec)



1.6
10.6
















TABLE 5B







COMPARATIVE SAMPLES









SAMPLE NO.













C591
C592
C636
C916
C918
















RESIN







PROPERTIES (first


reactor)


Flow Index, dg/min
0.57
0.50
0.4
0.65
0.66


I21


Melt Index, dg/min







I2


Density, g/cm3
0.9291
0.9244
0.9261
0.9238
0.9238


MFR







Titanium, ppmw
4.0
4.1
3.10
2.1
1.9


Aluminum ppmw
90.9
103.7
107.7
63.9
61.5


Al/Ti
40.4
45.5
62.4
53.9
56.4


Bulk Density, lb/ft3
23.3
21.5
17.7
15.9
15.9


APS, inches
0.026
0.025
0.0345
0.036
0.037


Fines, Wt % LT 120
1.2
1.1
1.9
1.6
1.3


Mesh
















TABLE 5C







COMPARATIVE SAMPLES









SAMPLE NO.













C591
C592
C636
C916
C918
















REACTION







CONDITIONS


(second reactor)


Temp. ° C.
94.9
94.9
99.9
94.9
94.9


Pressure, psig
392.6
392.6
380
388.0
386.8


C2 Part. Pressure,
64.8
70.4
75.3
84.8
91.0


psi


H2/C2 Molar Ratio
1.3
1.3
1.74800
1.3
0.8


C6/C2 Molar Ratio
0.07
0.03
0.0486
0.035
0.035


Ethylene lb/hr
17.8
19.8

25.2
30.3


Hexene lb/hr
1.3
0.7

0.8
0.9


Isopentane lb/hr



0.6
0.0


Nitrogen lb/hr



13.6
16.7


Ethylene Mol %



21.0
22.6


Hexene Mol %



0.7
0.8


Hydrogen Mol %



27.3
19.2


Isopentane Mol %



0.3
0.2


Nitrogen Mol %



49.3
55.8


E.B. Production
16.1
17.5
19.5
16.1
18.6


Rate, lb/hr


Bed Weight, lbs
90.1
89.5
152.3
97.9
98.0


Fluidized Bed


11.2
14.1
13.7


Density (lb/ft3)


Bed Volume, ft3


13.6
10.0
12.0


Residence Time, hr
2.1
2.0
3.5
1.92
1.82


Space Time Yield,
3.5
4.0
1.4
5.1
4.5


lb/hr/ft3


Superficial gas



1.8
1.7


velocity (ft/sec)
















TABLE 5D







COMPARATIVE SAMPLES








RESIN



PROPERTIES
SAMPLE NO.












(Blend)
C591
C592
C636
C916
C918















Flow Index, dg/min
9.0
8.5
8.9
9.9
9.7


I21 (G)


Melt Index, dg/min
0.15
0.1
0.38 (MI5)
0.13
0.14


I2 (G)


Density, g/cm3 (G)
0.9400
0.9403
0.9407
0.9399
0.9396


MFR (MI21/MI2)
61.1
69.4
23.4
73.9
67.6


(G)


(MI21/MI5)


Titanium, ppmw
2.4
2.5
1.88
1.3
1.1


(G)


Aluminum ppmw
57.9
56.0
74.9
58.1
46.5


(G)


Al/Ti (G)
43.2
39.9
71.2
80.5
75.5


Bulk Density, lb/ft3
26.3
24.6
20.4
19.6
18.7


(G)


APS, inches (G)
0.026
0.025
0.0302
0.033
0.034


Fines, Wt % less
2.0
1.7
3.7
2.3
1.9


than120 Mesh (G)


Split % by Energy
61.7
60.9

68.4
65.4


Balance(G)


Split % calculated
58.5
57.8
57.7
58.6
55.4


(G)





[Split % (calculated) = (weight of HMW/(sum weight (HMW + LMW))) × 100]













TABLE 5E







COMPARATIVE SAMPLES









SAMPLE NO.













C591
C592
C636
C916
C918
















MI2 - g/10 min (P)
0.14
0.13
0.0977
0.13
0.16


ASTM D-1238-04


MI5 - g/10 min (P)
0.53
0.45
0.382
0.48
0.60


ASTM D-1238-04


ASTM D-1238-04
1.8
1.6
1.51
1.71
2.13


MI21 - g/10 min(P)
9.4
8.2
9.45
9.14
10.59


ASTM D-1238-04


MFR (I21/I2) (P)
67.1
63.1
96.7
71.0
65.1


MFR (I21/I5) (P)
17.7
18.2
24.7
18.9
17.7


MFR (I10/I2) (P)
12.9
12.3
15.5
13.3
13.1


Density (g/cc) (P)
0.9403
0.9403
0.9425
0.9456
0.9446


ASTM D-790-00


IR structure (P)


Trans/1000 carbons
0
0
0.023
0.001
0.005


(P)


ASTM D-6248-2004


Vinyls/1000
0.135
0.126
0.219
0.17
0.2


carbons (P)


ASTM D-6248-2004


Methyls/1000
3.61
3.12
3.89
4.4
4


carbons (P)


ASTM D-2238-1999


Additive analysis


Irganox 1010 ppm
1324
1233
1824
1421
1462


Irgafos 168 ppm
1316
1365
2199
953
968


total


Irgafos 168 ppm
1080
1119
1994
533
654


Active


Irgafos 168 ppm
236
246
205
1486
1622


Inactive


Percent Active
0.82
0.82
90.68
64.1
59.7


I-168
















TABLE 5F







COMPARATIVE SAMPLES









SAMPLE NO.













C591
C592
C636
C916
C918
















RMS-100 Viscosity
9.00E+05
1.10E+06

1070000
866000


MPa · S at 0.01 sec−1


shear rate


RMS-800 Viscosity
25200
26100

24252
24463


MPa · S at 100 sec−1


shear rate


G′/G″ @ 0.01 sec−1
0.29
0.32

0.337
0.284


Shear Rate


G′/G″ @ 0.1 sec−1
0.42
0.45

0.467
0.421


Shear Rate


Viscosity ratio
35.7
42.1

44.1
35.4


0.01/100 data


Rheotens melt


13
11
10


strength (cN)


Rheotens Velocity



145
149


(mm)


DSC Melting Point
128.85
129.6
127.47
128.26
128.37


(Deg C.)


ASTM D-3418-03


Heat of Fusion (J/g)
180.2
173.6
190.8
184.7
180.6


ASTM D-3418-03


DSC Crystallization
115.45
115.45
116.41
116.05
116.1


point (Deg C.)


ASTM D-3418-03


Heat of
179.5
172.4
188.6
178
175.9


Crystallization (J/g)


ASTM D-3418-03


DSC Induction Time
43.62
39.9


(min)


ASTM D-3350-05


DSC Induction
237.86
245.58


Temp (Deg C.)


ASTM D-3350-05


C13 NMR Wt %
3.1
2.8
2.4
3.1
2.7


Hexene


ASTM D-5017-91
















TABLE 5G







COMPARATIVE SAMPLES









SAMPLE NO.













C591
C592
C636
C916
C918
















Atref HD fraction
74.7
77
73
69.2
68.3


(%)


Temperature
86.1
86.3
86.1
87.1
86.1


Minimum (C.)


SCB portion
14.6
12.3
14.6
17
14


SCB portion
50
56
56
55
60


minimum


temperature (C.)


SCB distribution Mv
92496
91775
112183
109150
119540


ATREF Purge (%)
10.7
10.7
12.4
13.8
17.7


Purge Mv
73084
86842
97678
84706
112700


ATREF Overall Mv
90419
91247
110384
105777
118329


Average


ATREF Dv viscosity -
0.054
0.018
0.041
−0.0032
0.021


temperature slope


(70° C. -90° C. region)


Triple Detector


Results


Conventional GPC


Mn
16690
19640
10890
17770
21120


Mw
194430
200670

161720
162700


Mz
808700
880800

707900
680800


Mw/Mn
11.6
10.2

9.1
7.7


Absolute GPC


Mn
20881
23343

17309
19200


Mw
215820
209010
241400
157960
168500


Mw (abs)/Mn abs
10.3
9.0
22.2
9.1
8.8


Mz (BB)
845200.0
805000.0
1290000
590100
645500


Mz (abs)
965500
896400

620400
732400


Mz + 1 (BB)
1647200.0
1536400.0
2504000.0
1114200
1196200


Mz (abs)/Mw
4.47
4.29
5.3
3.9
4.3


Mw (abs)/Mw
1.11
1.04


(GPC)
















TABLE 5H







COMPARATIVE SAMPLES









SAMPLE NO.












Plaque Properties
C591
C592
C636
C916
C918















PENT (2.4 MPa)
18047
>19320
1687
12880
>13,181


Hrs

(discontinued)

(discontinued)
(on test)


ASTM D-1473-01


RCP Gc @ 23 C.
127
175
176.1
194.5
175.7


from PENT plaque


milled to 2 mm thick


samples (KJ/m2)


Modified (2 mm)


ASTM F-2231-02


RCP Gc @ 23 C.


from PENT plaque


milled to 3 mm thick


samples (KJ/m2)


ASTM F-2231-02


Flexural Modulus
134000
135000
144400
151000
148770


(psi) @ 0.5 inches/min


ASTM D-790-03


SD



8666
5640


Secant Modulus
95000
100000

102000
100075


(psi) 2% @ 0.5 inches/min


ASTM D-790-03


SD



920
1675


Secant Modulus
114000
120000

122300
120000


(psi) 1% @ 0.5 inches/min


ASTM D-790-03


SD



1473
281


Tensile Strength
5320
5470
4764
5074
5554


(PSI)


ASTM D638-03


SD



444
300


% Elongation
880
730
752
740
630


ASTM D638-03


SD



55
118


Yield Strength (psi)
2440
2860
2700
2448
2572


ASTM D638-03


SD



65
163


Yield Strain (%)
15.7?
11?
5.9
4
5.6


ASTM D638-03


SD



0.25
3.6
















TABLE 5I







COMPARATIVE SAMPLES









SAMPLE NO.












Burst Properties
C591
C592
C636
C916
C918















10**5 intercept at
NA
NA
NA
NA
1328


23 C. (psi)


ASTM D-1598-02


ASTM D-2837-04


10**5 intercept at
Failed
Failed
~940
Failed
952


60 C., (psi)


ASTM D-1598-02


ASTM D-2837-04


Hours on test at 60 C.




7388


90 C. validation test
NA
NA

NA


(690 psi Hoop stress


for >3800 hours)


PPI TR #3 Section


F.4.2.1





NA = Not Applicable













TABLE 6A







COMPARATIVE SAMPLES









SAMPLE NO.













C919
C920
C921
C923
C924
















Type
Precursor
Precursor
Precursor
Precursor
0017







reduction


First Reactor


REACTION


CONDITIONS


Temp. ° C.
80.0
80.0
80.0
80.0
80.0


C2 Part. Pressure, psi
30.8
36.8
33.5
26.5
38.8


H2/C2 Molar Ratio
0.012
0.034
0.028
0.034
0.027


C6/C2 Molar Ratio
0.115
0.124
0.112
0.099
0.114


Ethylene lb/hr
27.5
26.8
27.5
26.9
27.0


Hexene lb/hr
1.8
2.1
1.8
1.5
1.9


Hydrogen mlb/hr
2.7
7.1
5.4
5.2
5.4


Isopentane lb/hr







Nitrogen lb/hr
4.6
4.3
4.4
4.1
3.8


Ethylene Mol %
9.8
11.8
10.7
8.5
12.4


Hexene Mol %
1.1
1.4
1.2
0.8
1.4


Hydrogen Mol %
0.1
0.4
0.3
0.3
0.3


Isopentane Mol %
8.0
8.0
8.0
8.0
8.0


Nitrogen Mol %
79.7
78.5
79.2
82.3
78.2


Cat cc/hr
14.4
14.4
14.4
14.4
15.4


E.B. Production Rate,
34.7
34.8
34.8
35.0
35.1


lb/hr


Bed Weight, lbs
68.7
68.5
68.5
68.5
68.3


FBD(lb/ft3)
12.3
12.3
12.3
12.7
11.7


Bed Volume, ft3
11.64
11.64
11.64
11.64
12.64


Residence Time, hr
2.0
2.0
2.0
2.0
1.9


STY, lb/hr/ft3
3.0
3.0
3.0
3.0
2.8


SGV (ft/sec)
11.6
11.6
11.6
11.6
12.6
















TABLE 6B







COMPARATIVE SAMPLES









SAMPLE NO.













C919
C920
C921
C923
C924
















RESIN







PROPERTIES (First


reactor)


Flow Index, dg/min
0.26
0.87
0.66
0.56
0.71


I21


Melt Index, dg/min







I2


Density, g/cm3
0.9179
0.9183
0.9194
0.9206
0.9205


MFR







Titanium, ppmw
1.7
1.8
1.8
2.3
1.6


Aluminum ppmw
60.6
65.0
71.7
65.5
71.6


Al/Ti
62.3
63.4
71.9
50.1
81.0


Bulk Density, lb/ft3
16.1
15.8
15.3
16.4
15.4


APS, inches
0.041
0.041
0.039
0.038
0.041


Fines, Wt % LT 120
1.5
1.0
1.2
0.9
0.4


Mesh
















TABLE 6C







COMPARATIVE SAMPLES









SAMPLE NO.













C919
C920
C921
C923
C924
















REACTION







CONDITIONS


(Second reactor)


Temp. ° C.
94.9
94.9
95.0
94.9
95.0


Pressure, psig
387.7
386.6
386.7
342.6
342.7


C2 Part. Pressure, psi
123.6
100.1
113.4
70.1
127.1


H2/C2 Molar Ratio
0.8
0.5
0.5
1.3
0.5


C6/C2 Molar Ratio
0.013
0.011
0.011
0.01
0.01


Ethylene lb/hr
37.8
33.5
37.7
27.5
36.7


Hexene lb/hr
0.5
0.4
0.4
0.3
0.4


Isopentane lb/hr
1.0
1.0
1.0
1.0
2.0


Nitrogen lb/hr
13.5
17.6
17.4
21.2
13.1


Ethylene Mol %
30.7
24.9
28.2
19.6
35.6


Hexene Mol %
0.4
0.3
0.3
0.2
0.4


Hydrogen Mol %
26.0
12.4
14.1
25.5
17.7


Isopentane Mol %
0.4
0.3
0.3
0.4
0.3


Nitrogen Mol %
41.8
61.5
56.1
53.8
45.6


E.B. Production Rate,
22.9
20.7
25.1
16.6
24.1


lb/hr


Bed Weight, lbs
98.6
98.6
99.6
98.0
98.4


Fluidized Bed Density
13.8
12.7
13.0
14.6
14.0


(lb/ft3)


Bed Volume, ft3
13.0
13.0
13.0
13.0
14.0


Residence Time, hr
1.71
1.78
1.66
1.90
1.66


Space Time Yield,
4.4
4.3
4.6
4.0
4.2


lb/hr/ft3


Superficial gas
1.7
1.7
1.7
1.6
1.6


velocity (ft/sec)
















TABLE 6D







COMPARATIVE SAMPLES









SAMPLE NO.













C919
C920
C921
C923
C924
















RESIN







PROPERTIES


(Blend)


Flow Index, dg/min
8.6
8.6
9.2
7.5
9.0


I21 (G)


Melt Index, dg/min
0.09
0.17
0.17
0.11
0.17


I2 (G)


Density, g/cm3 (G)
0.9405
0.9371
0.9397
0.9392
0.9396


MFR (MI21/MI2) (G)
100.6
49.6
54.3
70.2
54.4


Titanium, ppmw (G)
1.0
1.1
0.9
1.6
0.9


Aluminum ppmw (G)
41.8
50.6
41.4
54.6
46.3


Al/Ti (G)
77.1
80.3
85.3
62.4
91.9


Bulk Density, lb/ft3
18.7
17.9
17.9
19.5
18.9


(G)


APS, inches (G)
0.036
0.038
0.038
0.033
0.039


Fines, Wt % less
1.8
1.2
1.5
1.8
0.6


than 120 Mesh (G)


Split % by Energy
60.3
62.6
58.1
67.8
59.3


Balance (G)


Split % calculated (G)
47.9
54.8
50.5
60.5
51.6


MI2 - g/10 min (P)
0.10
0.19
0.19
0.10
0.17


ASTM D-1238-04


MI5 - g/10 min (P)
0.42
0.67
0.71
0.46
0.66


ASTM D-1238-04


MI10 - g/10 min (P)
1.68
2.16
2.36
1.53
2.20


ASTM D-1238-04


MI21 - g/10 min (P)
9.14
9.84
11.06
8.13
10.58


ASTM D-1238-04


MFR (I21/I2) (P)
90.7
51.0
58.3
81.1
61.6


MFR (I21/I5) (P)
21.6
14.7
15.6
17.7
16.1


MFR (I10/I2) (P)
16.6
11.2
12.4
15.2
12.8





[Split % (calculated) = (weight of HMW/(sum weight (HMW + LMW))) × 100]













TABLE 6E







COMPARATIVE SAMPLES









SAMPLE NO.













C919
C920
C921
C923
C924
















Density (g/cc) (P)
0.9457
0.9424
0.9455
0.9451
0.9447


ASTM D-792-00


IR structure (P)


Trans/1000
0.034
0.062
0.04
0.02
0.036


carbons(P)


ASTM D-6248-2004


Vinyls/1000 carbons
0.2
0.16
0.18
0.17
0.18


(P)


ASTM D-6248-2004


Methyls/1000
4.4
1.5
4
4.7
4.2


carbons (P)


ASTM D-2238-1999


Additive analysis


Irganox 1010 ppm
1500
1494
1486
1452
1642


Irgafos 168 ppm total
918
760
733
823
836


Irgafos 168 ppm
694
907
923
826
1049


Active


Irgafos 168 ppm
1612
1667
1656
1649
1885


Inactive


Percent Active I-
56.9
45.6
44.3
49.9
44.4


168


RMS-100 Viscosity
150000
74500
75400
132000
92700


MPa · S at 0.01 sec−1


shear rate


RMS-800 Viscosity
2379
2616
2467
2649
2545


MPa · S at 100 sec−1


shear rate


G′/G″ @ 0.01 sec−1
0.327
0.295
0.308
0.397
0.384


Shear Rate


G′/G″ @ 0.1 sec−1
0.563
0.404
0.422
0.511
0.48


Shear Rate


Viscosity ratio
63.1
28.5
30.6
49.8
36.4


0.01/100 data


Rheotens melt
12.5
9.5
9.5
12.5
10


strength (cN)


Rheotens Velocity
130
150
160
130
125


(mm)
















TABLE 6F







COMPARATIVE SAMPLES









SAMPLE NO.













C919
C920
C921
C923
C924
















DSC Melting Point
129.3
129.22
129.82
128.79
129.28


(Deg C.)


ASTM D-3418-03


Heat of Fusion (J/g)
187.2
174.9
177.5
180.3
180.8


ASTM D-3418-03


DSC Crystallization
116.75
116.33
116.49
116.32
117.53


point (Deg C.)


ASTM D-3418-03


Heat of Crystallization
175.6
169.8
170.9
175.5
180


(J/g)


ASTM D-3418-03


DSC Induction Time


(min)


ASTM D-3350-05


DSC Induction Temp


(Deg C.)


ASTM D-3350-05


C13 NMR Wt %
2.8
3.6
2.8
3


Hexene


ASTM D-5017-91


Branches/1000 C in


Backbone


ASTM D-5017-91


ATREF HD fraction
72.2
67.6
74.5
72.1
72.3


(%)


Temperature Minimum
87
87.4
86.6
86
86


(° C.)


SCB portion
13.9
17.6
12.8
15.2
13.2


SCB portion minimum
55
35
55
48
55


temperature (° C.)


SCB distribution Mv
118808
117914
104429
100613
76229


ATREF Purge (%)
13.9
14.8
12.7
12.7
14.5


Purge Mv
99009
104622
85525
79988
63014


ATREF Overall Mv
116056
115947
102028
97994
74313


Average


ATREF Dv viscosity -
−0.0027
0.0063
0.00031
−0.00078
−0.0011


temperature slope


(70° C. -90° C. region)
















TABLE 6G







COMPARATIVE SAMPLE









SAMPLE NO.













C919
C920
C921
C923
C924
















Triple







Detector


Results


Conventional


GPC


Mn
21660
29250
28640
22120
31000


Mw
196560
133280
170000
200480
186380


Mz
885000
453400
679700
827900
776200


Mw/Mn
9.1
4.6
5.9
9.1
6.0


Absolute


GPC


Mn
20500
29900
29900
21640
30733


Mw
199290
163170
191960
200750
194260


Mw (abs)/
9.7
5.5
6.4
9.3
6.3


Mn abs


Mz(BB)
829000
558100
704000
790200
759200


Mz (abs)
811200
927600
867100
785600
865000


Mz + 1 (BB)
1540300
1108400
1356800
1467100
1440300


Mz (abs)/
4.1
5.7
4.5
3.9
4.5


Mw
















TABLE 6H







COMPARATIVE SAMPLE









SAMPLE NO.












Plaque Properties
C919
C920
C921
C923
C924















PENT (2.4 MPa)
>13513
>13478
>13274
12768
12314


Hrs
(on test)
(on test)
(on test)
(discontinued)
(discontinued)


ASTM D-1473-01


RCP Gc @ 23 C. from
204.9
193.4
206
193.4
204.9


PENT plaque milled


to 2 mm thick


samples (KJ/m2)


Modified (2 mm)


ASTM F-2231-02


RCP Gc @ 23 C. from


PENT plaque milled


to 3 mm thick


samples (KJ/m2)


ASTM F-2231-02


Flexural Modulus
153800
141250
151000
144000
139300


(psi) @ 0.5 inches/min


ASTM D-790-03


SD
3650
2920
8520
6580
8540


Secant Modulus (psi)
101600
93150
101700
98000
95400


2% @ 0.5 inches/min


ASTM D-790-03


SD
1718
1400
1907
2626
2685


Secant Modulus (psi)
122200
112300
122000
117500
114300


1% @ 0.5 inches/min


ASTM D-790-03


SD
2093
1310
2660
3978
4062


Tensile Strength (PSI)
5376
5310
5040
4980
5080


ASTM D-638-03


SD
134
150
412
140
395


% Elongation
620
682
725
590
695


ASTM D-638-03


SD
54
37
35
80
50


Yield Strength (psi)
2628
2330
2525
2438
2544


ASTM D-638-03


SD
115
48
59
27
52


Yield Strain (%)
6.4
4.6
4.56
4.7
4.72


ASTM D-638-03


SD
5.3
0.09
0.23
0.17
0.38
















TABLE 6I







COMPARATIVE SAMPLES









SAMPLE NO.












Burst Properties
C919
C920
C921
C923
C924





10**5 intercept at 23 C.
NA
NA
NA
NA
NA


(psi)


ASTM D-1598-02


ASTM D-2837-04


10**5 intercept at 60 C.,
Failed
Failed
Failed
Failed
Failed


(psi)


ASTM D-1598-02


ASTM D-2837-04


90 C. validation test
NA
NA
NA
NA
NA


(690 psi Hoop stress


for >3800 hours)


PPI TR #3 Section


F.4.2.1





NA = Not Applicable













TABLE 7A







COMPETITIVE SAMPLES









SAMPLE NO.










COM049
COM769





Type
Solvay-Fortiflex
Chevron Phillips


Info
K-38-20-160
TR-418Q


MI2 - g/10 min (P)
0.22
0.14


ASTM D-1238-04




MI5 - g/10 min (P)
1.05
0.76


ASTM D-1238-04




MI10 - g/10 min (P)
3.85
3.26


ASTM D-1238-04




MI21 - g/10 min (P)
19.9
15.4


ASTM D-1238-04




MFR (I21/I2) (P)
90.5
110


MFR (I21/I5) (P)
19.0
20.3


MFR (I10/I2) (P)
17.5
23.3


Density (g/cc) (P)
0.9422
0.9398


ASTM D-792-00




Additive analysis




Irganox 1010 ppm

1312


Irgafos 168 ppm total

700


Irgafos 168 ppm Active

660


Irgafos 168 ppm Inactive

40


Percent Active I-168

0.94


RMS-100 Viscosity MPa · S
91500
116000


at 0.01 sec-1 shear rate




RMS-800 Viscosity MPa · S at 100

1870


sec-1 shear rate




G′/G″ @ 0.01 sec-1 Shear Rate

0.63


G′/G″ @ 0.1 sec-1 Shear Rate

0.68


Viscosity ratio 0.01/100 data

62


Rheotens melt strength (cN)
13
















TABLE 7B







COMPETITIVE SAMPLES cont.









SAMPLE NO.










COM049
COM769












DSC Melting Point (Deg C.)
126.63



ASTM D-3418-03




Heat of Fusion (J/g)
181.5



ASTM D-3418-03




DSC Crystallization point (Deg C.)
114.57



ASTM D-3418-03




Heat of Crystallization (J/g)
164.6



ASTM D-3418-03




DSC Induction Time (min)




ASTM D-3350-05




DSC Induction Temp (Deg C.)




ASTM D-3350-05




C13 NMR Wt % Hexene
3.2
3.7


ASTM D-5017-91




Branches/1000 C. in Backbone




ASTM D-5017-91




Atref HD fraction (%)
70.5
68.8


Temperature Minimum (C.)
86
87


SCB portion
22.1
19


SCB portion minimimu temperature (C.)
55
62


SCB distribution Mv
98970
130026


Aterf Purge (%)
7.4
12.2


Purge Mv
71715
93577


Atref Overall Mv Average
96953
125579


Atref Dv viscosity - temperature slope
0.04
0.018


(70° C.-90° C. region)




Triple Detector Results




Conventional GPC




Mn
14900
10800


Mw

200000


Mz

1555000


Mw/Mn

18.5


Absolute GPC




Mn

11000


Mw
145800
200500


Mw (abs)/Mn abs
9.79
18.6


Mz (BB)
713400
1533000


Mz (abs)
1480000
1482000


Mz + 1 (BB)

3610000.0


Mz (abs)/Mw
4.89
7.4


Mw (abs)/Mw (GPC)

1.0
















TABLE 7C







COMPETITIVE SAMPLES cont.









SAMPLE NO.










COM049
COM769












Plague Properties




PENT (2.4 MPa) Hrs
2890
8625


ASTM D-1473-01




RCP Gc @ 23 C. from PENT plaque milled to
120
53


2 mm thick samples (KJ/m2)




Modified (2 mm) ASTM F-2231-02




RCP Gc @ 23 C. from PENT plaque milled to




3 mm thick samples (KJ/m2)




ASTM F-2231-02




Flexural Modulus (psi) @ 0.5 inches/min
130700
126000


ASTM D-790-03




SD




Secant Modulus (psi) 2% @ 0.5 inches/min

89400


ASTM D-790-03




SD




Secant Modulus (psi) 1% @ 0.5 inches/min

105000


ASTM D-790-03




SD




Tensile Strength (PSI)
4290
4425


ASTM D-638-03




SD




% Elongation
822
780


ASTM D-638-03




SD




Yield Strength (psi)
2633
2720


ASTM D-638-03




SD




Yield Strain (%)
7.1



ASTM D-638-03




SD




Burst Properties




10**5 intercept at 23 C. (psi)
>1260
>1260


ASTM D-1598-02




ASTM D-2837-04




10**5 intercept at 60 C., (psi)
>960
>960


ASTM D-1598-02




ASTM D-2837-04




Hours on test at 60 C.




90 C. validation test (690 psi Hoop stress for




>3800 hours)




PPI TR #3 Section F.4.2.1










Scale-Up Polymerizations


Two scale-up polymerizations (inventive examples) are shown in tables 8A and 8B.


Preparation of Catalyst Precursor


A titanium trichloride catalyst precursor was prepared in an approximately 7,500 liter glass lined vessel, equipped with pressure and temperature control, and a turbine agitator. A nitrogen atmosphere (<5 ppm H2O) was maintained at all times. Tetrahydrofuran (10,500 lbs, 4,800 kg, <400 ppm H2O) were added to the vessel. The tetrahydrofuran was recovered from a closed cycle dryer, and contained approximately 0.1 percent Mg and 0.3 percent Ti. An “11 percent THF solution” of triethylaluminum was added to scavenge residual water. The reactor contents were heated to 40° C., and 13.7 lbs (6 kg) of granular magnesium metal (particle size 0.1-4 mm) was added, followed by 214.5 lbs (97.3 kg) of titanium tetrachloride added over a period of one-half hour.


The mixture was continuously agitated. The exotherm resulting from the addition of titanium tetrachloride caused the temperature of the mixture to rise to approximately 44° C. The temperature was then raised to 70° C., and held at that temperature for approximately four hours, then cooled to 50° C. At the end of this time, 522 pounds (238 kg) of magnesium dichloride were added, and heating initiated to raise the temperature to 70° C. The mixture was held at this temperature for another five hours, then cooled to 35° C., and filtered through a 100 mesh (150 μm) filter to remove solids.


Fumed silica (CAB-O-SIL™ TS-610, manufactured by the Cabot Corporation) (811 lbs, 368 kg) was added to the above precursor solution over a period of one hour. The mixture was stirred by means of a turbine agitator during this time, and for 4 hours thereafter, to thoroughly disperse the silica. The temperature of the mixture was held at 40° C. throughout this period, and a dry nitrogen atmosphere was maintained at all times. The resulting slurry was spray dried using an 8-foot diameter, closed cycle spray dryer, equipped with a rotary atomizer. The rotary atomizer was adjusted to give catalyst particles with a D50 on the order of 20-30 μm. The scrubber section of the spray dryer was maintained at approximately +5 to −5° C.


Nitrogen gas was introduced into the spray dryer at an inlet temperature of 140 to 165° C., and was circulated at a rate of approximately 1000-1800 kg/hour. The catalyst slurry was fed to the spray dryer at a temperature of about 35° C., and a rate of 65-150 kg/hour, or sufficient to yield an outlet gas temperature in the range of 100-125° C. The atomization pressure was maintained at slightly above atmospheric. The resulting catalyst particles are mixed with mineral oil (Kaydol™ 350, available from Witco Corporation), under a nitrogen atmosphere, in a 400 liter glass lined vessel, equipped with a turbine agitator, to form a slurry containing approximately 28 percent of the catalyst precursor.


Catalyst Precursor Partial Pre-Activation


The mineral oil slurry of precursor was partially activated (0017 reduction) by contact at room temperature with an appropriate amount of a 50 percent mineral oil solution of tri-n-hexyl aluminum (TNHA). The catalyst precursor slurry was pre-contacted with the activator, and fed through a Kenics mixer to provide mixing prior to feeding to the reactor.


Polymerization


As shown in Tables 8A and 8B, ethylene was copolymerized with 1-hexene in two fluidized bed reactors. Each polymerization was continuously conducted, after equilibrium was reached, under the respective conditions, as set forth in Tables 8A and 8B. Polymerization was initiated in the first reactor, by continuously feeding the catalyst (Ziegler/Natta catalyst) and cocatalyst (trialkyl aluminum (triethyl aluminum or TEAL)) into a fluidized bed of polyethylene granules, together with ethylene, 1-hexene and hydrogen. The resulting copolymer, mixed with active catalyst, was withdrawn from the first reactor, and transferred to the second reactor, using second reactor gas as a transfer medium. The second reactor also contained a fluidized bed of polyethylene granules. Ethylene, 1-hexene, and hydrogen were introduced into the second reactor, where the gases come into contact with the polymer and catalyst from the first reactor. Inert gases, nitrogen and isopentane, made up the remaining pressure in both the first and second reactors. In the second reactor, the cocatalyst was again introduced. The final product blend was continuously removed. In the second scale-up run, the second reactor (2B) was operated in condensing mode. This resulted in an improvement in reactor operation through a significant reduction in the level of static build-up in the reactor, and a reduction in the tendency for resin to be drawn toward the reactor walls.











TABLE 8A









SAMPLE NO.












1A (First
1B (Second
2A (First
2B (Second



Reactor)
Reactor)
Reactor)
Reactor)















Catalyst
0017 re-

0017 re-



Modification
duction

duction


Temp. ° C.
80
95
80
95


Pressure (psig)
283
353
281
345


C2 Part. Pressure,
36.2
89.7
39.7
79.5


psi


H2/C2 Molar Ratio
0.032
0.6
0.029
0.60


C6/C2 Molar Ratio
0.058
0.026
0.059
0.026


N2 Mol %
74.6
52.8
72.5
51.4


H2 Mol %
0.386
14.6
0.396
13.2


C4H4 Mol %
12.1
24.4
13.4
22.1


C2H6 Mol %
0.941
1.53
0.907
1.48


IC5 Mol %
10.77
5.94
11.93
10.91


C6H12 Mol %
0.7
0.632
0.79
0.571


Teal Flow (lbs/hr)
6.8
2.5
8.9
3.4


Production Rate,
37.7
37
46.4
42.7


Mlb/hr


Catalyst Feed
12.2

15.9



(lbs/hr)


TnHal Feed lb/hr)
1.23

1.60



TnHal/THF
17

17



C2 Feed (Mlbs/hr)
36.6
36.6
45.1
42.2


Total C6 Feed
1154
624
1413
738


(lbs/hr)


H2 Feed (lbs/hr)
0.62
26.3
0.64
26.4


N2 Feed (lbs/hr)
201
26
278
31


Total IC5 Feed to
941
0
1508
558


Rx (lbs/hr)


Vent Flow (lbs/hr)
0
692
0
967


Bed Weight (Mlbs)
88.4
166
85.1
175


Upper FBD (lbs/ft3)
13
15.4
12.9
16.5


Lower FBD (lbs/ft3)
15.2
18.6
14.4
19.3


Bed Level (ft)
32.6
47.2
38.7
48.0


















TABLE 8B









SAMPLE NO.












1A (First
1B (Second
2A (First
2B (Second



Reactor)
Reactor)
Reactor)
Reactor)















Residence Time
2.3
2.2
1.8
2.0


(hr)


STY (lb/hr/ft3)
6.5
4.2
7.8
4.7


SGV (ft/s)
1.69
2.03
1.72
1.83


Dewpoint (° C.)
51.4
40.7
54.2
55.9


Inlet Temp. (° C.)
40.9
56.9
39.2
51.9


Wt % Condensing
7.07
0
10.59
3.71


Split
0.504
0.496
0.521
0.479


C2 Split
0.5
0.5
0.516
0.484


Ti (ppmw)
2.57
1.25
3.11
1.65


Al/Tl
73.8
74.5
61.0
62.3


Melt Index (I5)

0.66

0.65


Flow Index (I21)
0.57
10.14
0.55
10.10


MFR (I21/I5)

15.4

15.5


Density (g/cc)
0.9243
0.9392
0.9248
0.9396





[Split % (calculated) = weight of HMW/(sum weight (HMW + LMW)) × 100]






Each blend has a single peak in an ATREF profile eluting above 30° C., and has a coefficient of viscosity average molecular weight (CMv) less than −0.0032 in the log(calculated Mv) versus elution temperature, said CMv calculated in the range of elution temperatures from 70° C. to 90° C., and wherein Mv is the viscosity average molecular weight.


Film Data


Inventive composition D20 comprises a blend containing a high molecular weight ethylene/hexene-1 interpolymer and a low molecular weight ethylene/hexene-1 interpolymer.


The high molecular weight ethylene/hexene-1 interpolymer is a heterogeneously branched linear interpolymer, and has a density of 0.9243 g/cc, and a high load melt index (I21) of 0.57 g/10 min (direct measurement).


The low molecular weight ethylene/hexane-1 interpolymer is heterogeneously branched linear interpolymer, and has a density in the range of 0.949-0.955 g/cc, and a melt index (I2) in the range of 15-25 g/10 min.


The blend has a single peak in an ATREF profile eluting above 30° C., and has a coefficient of viscosity average molecular weight (CMv) less than −0.0032 in the log(calculated Mv) versus elution temperature, said CMv calculated in the range of elution temperatures from 70° C. to 90° C., and wherein Mv is the viscosity average molecular weight.


A description of the reaction conditions for the D20 blend is shown in Tables 8A and 8B. Some properties of the D20 resin are shown in Table 9. The ATREF-DV overlay profile for the D20 blend is shown in FIG. 29.


The D20 composition was fabricated into a three films (D20-1 to D20-3) on a standard smooth barrel extruder. The extrusion conditions are shown in Table 10.


Film properties are shown in Tables 11 and 12. Film tensile properties were compared against a film prepared from a comparative, unimodal, Cr catalyzed ethylene/1-hexene, copolymer (D25).


The two films, D20-1 (5 mils) and D20-2 (5 mils), had the following properties: a MD Tear of 131 g/mil and 140 g/mil, respectively, a CD Tear of 460 g/mil and 390 g/mil, respectively, a Dart Impact that exceeded the A scale, and a Normalized Dart Impact of 81.5 g/mil and 85.1 g/mil, respectively, on the “B” scale (1 mil=0.001 inch, and 1 inch=25.4 mm).


The film D20-3 (9 mils) had the following properties: a MD tear of 190 g/mil, a CD tear of 260 g/mil, a Dart Impact that exceeded the “A” scale, and a Normalized Dart Impact of 104.8 g/mil on the “B” scale.


For each film, unexpectedly superior properties were demonstrated. The films had good MD Tear and Dart Impact. These properties are especially needed in heavy duty shipping sacks (HDSS), where high stiffness, good Tear Resistance and good Dart Impact are required.


For “drip irrigation tubing,” typical industry requirements for 4 to 6 mil thick film are as follows: Yield Strength CD (ASTM 882) from 3350 to 4250 psi, and Yield Strength MD (ASTM 882) from 2750 to 3450 psi. As shown in Table 12B, none of the comparative films (D25-1 and D25-3), at 5 mils, met the CD yield strength requirement. However, as shown in Table 12A, the inventive films (D20-1 and D20-2), at 5 mils, met the required CD yield strength, and met, or came very close to, the required MD yield strength.









TABLE 9





Basic Property Data of D20 Resin and D25 Resin




















ASTM Test
Units
D20
D25





Basic Property Data


MI2
D-1238-04
g/10 min
0.17
0.22


MI5
D-1238-04
g/10 min
0.63
1.1


MI10
D-1238-04
g/10 min
2.2
4.4


MI21
D-1238-04
g/10 min
10.7
22.5


MI21/MI2


62.9
102


MI21/MI5


17.0
20.5


MI10/MI2


12.9


Density (ASTM)
D-792-00
g/cc
0.9406




Corrected for
0.9393
0.9398




the additive




contribution


Flexural Modulus @ 5%
D-790-99
psi
138000


Secant Modulus @ 2%
D-790-99
psi
95000


Secant Modulus @ 1%
D-790-99
psi
113500


Tensile Strength @ Break
D-638-03
psi
5040


% Elongation @ break
D-638-03

950


Yield Strength
D-638-03
psi
2930


% Elongation @ yield
D-638-03

7.1


Irganox 1010

ppm
1500


Irgafos 168

ppm
1500


UV 3529

ppm
1670


UV 531

ppm
560


Conventional GPC Data


Mn


25000


Mw


197000


Mw/Mn


7.9


Mz


865000


Absolute GPC Data


Mn


24500


Mw


222000


Mw/Mn


9.1


Mz(BB)


1114000


Mz(abs)


1461000


Mz + 1 (BB)


2513000


Mz/Mw


6.58


g′


0.986














Test
Units
D20





Basic Property Data


DMS Viscosity


0.01585 sec−1

Pa-s
57300


0.1 sec−1

Pa-s
40000


100 sec−1

Pa-s
2028


Ratio 0.01585/100

Pa-s
28.2


Ratio 0.1/100

Pa-s
19.7


DSC


Melting Point (° C.)


127.7


Enthalpy (J/g)


184.7


Crystallization Point (° C.)


116


Enthalpy (J/g)


183.9


OIT @ 210 (° C.)


>100 minutes


Thermal Stability (need >220 (° C.))
ASTM D-

248.6



3350-02


ATREF


ATREF HD fraction (%)


75.2


Temperature Minimum (° C.)


86


SCB portion


13.7


SCB portion minimum


45


temperature (° C.)


SCB distribution Mv


162200


ATREF Purge (%)


11.1


Purge Mv


153400


ATREF Overall Mv Average


161200


ATREF Dv viscosity - temperature


−0.012


slope (70-90° C. region)
















TABLE 10







Extrusion Conditions for D20 Films


Extruder 2.5 inch


Screw Davis Standard


Barrier II


Die Diameter 6 inches


Die Gap 70 mils











Barrel Zone






Temperature
Set
Actual
Actual
Actual















Barrel 1
F.
375
376
375
375


Barrel 2
F.
435
435
435
435


Barrel 3
F.
420
420
421
420


Barrel 4
F.
405
405
405
405


Barrel 5
F.
405
404
406
404


Screen Changer
F.
420
420
420
420


Adapter
F.
420
421
418
419


Rotator
F.
420
424
430
412


Lower Die
F.
420
419
421
419


Upper Die
F.
420
419
423
420


Output Rate
lbs/hr

101.1
101.9
101.9


RPM


51.5
51.5
51.5


Rate/RPM
lbs/hr/RPM

1.96
1.98
1.98


Barrel Pressure
psi

2450
2540
2680


P1


Barrel Pressure
psi

3140
3420
3030


P2


Barrel Pressure
psi

4250
4350
4440


P3


Screen Changer
psi

4850
4740
4870


Adapter
psi

1910
2010
1990


Melt Temperature
F.

473
472
473
















TABLE 11A







D20 Film Data












Product
Test
Units
D20-1
D20-2
D20-3















Gage

mils
5
5
9


BUR


2
2.1
2.1


MI2
ASTM D-
g/10 min
0.17
0.17
0.17



1238-04


MI21
ASTM D-
g/10 min
10.7
10.7
10.7



1238-04


MFR


62.9
62.9
62.9


(MI21/MI2)


Density
ASTM D-
g/cc
0.9393
0.9393
0.9393



792-00


COF O/I
ASTM D-



1894-06


Kinetic

Dimen-
0.308
0.32
0.279




sionless


Static

Dimen-
0.348
0.347
0.408




sionless


Dart A Scale
ASTM D-
g
No Fail
No Fail
No



1709-04



Fail


Dart B
ASTM D-
g
428
404
996


scale**
1709-04


Actual


5.25
4.75
9.5


Thickness


Normalized

g/mil
81.5
85.1
104.8


Dart B


Elmendorf


Tear


CD (or TD)
ASTM D-
g/mil
460
390
260



1922-06a


MD
ASTM D-
g/mil
131
140
190



1922-06a


MD/CD


0.28
0.36
0.73


Gloss
ASTM D-
%
6.6
6.6
7.1



2457-03


Haze
ASTM D-
%
77
76
80



1003-00


Puncture
ASTM D-
(Ft-Lb)/
76.5
71.8
29.8



5748-07
in3





**B scale dart impact - sample did not fail on the A scale.













TABLE 11B







D25 Comparative Film Data












Product
Test
Units
D25-1
D25-2
D25-3















Gage

mils
5
9
5


BUR


2
2.1
2.1


MI2
ASTM D-
g/10 min
0.22
0.22
0.22



1238-04


MI21
ASTM D-
g/10 min
22.5
22.5
22.5



1238-04


MFR


102
102
102


(MI21/MI2)


Density
ASTM D-
g/cc
0.9398
0.9398
0.9398



792-00


COF O/I
ASTM D-



1894-06


Kinetic

Dimen-
0.336
0.252
0.271




sionless


Static

Dimen-
0.375
0.277
0.237




sionless


Dart A Scale
ASTM D-
g
340
700
320



1709-04


Dart B Scale
ASTM D-
g






1709-04


Actual


4.8
9
4.8


Thickness


Normalized

g/mil
70.8
77.8
66.7


Dart A


Elmendorf


Tear


CD (or TD)
ASTM D-
g/mil
575
389
570



1922-06a


MD
ASTM D-
g/mil
77
124
90



1922-06a


MD/CD


0.13
0.32
0.16


Gloss
ASTM D-
%
4.6
5
5.2



2457-03


Haze
ASTM D-
%
83.5
84.4
84.1



1003-00


Puncture
ASTM D-
(Ft-Lb)/






5748-07
in3
















TABLE 12A







Film Tensile Properties
















Industry








Re-





quire-


Product
Test
Units
ments
D20-1
D20-2
D20-3
















Nominal Gage

mils
4-6 mils
5
5
9


BUR



2
2.1
2.1


Tensile


Properties


Ultimate
ASTM D-
psi

6500
7000
5270


Tensile CD
882-02


Ultimate
ASTM D-
psi

7520
5430
6560


Tensile MD
882-02


% Elongation
ASTM D-


750
695
745


CD
882-02


% Elongation
ASTM D-


600
580
770


MD
882-02


Yield Strength
ASTM D-
psi
3350-
3380
3420
3120


CD
882-02

4250


Yield Strength
ASTM D-
psi
2750-
2990
2740
2900


MD
882-02

3450


Secant
ASTM D-
psi

92000
95500
85000


Modulus 1%
882-02


CD


Secant
ASTM D-
psi

74000
76500
69000


Modulus 2%
882-02


CD


Secant
ASTM D-
psi

76500
80000
77000


Modulus 1%
882-02


MD


Secant
ASTM D-
psi

63000
65000
63500


Modulus 2%
882-02


MD
















TABLE 12B







Film Tensile Properties
















Industry








Re-





quire-


Product
Test
Units
ments
D25-1
D25-2
D25-3
















Nominal Gage

mils
4-6 mils
5
9
5


BUR



2
2.1
2.1


Tensile


Properties


Ultimate
ASTM D-
psi

5250
5120
4910


Tensile CD
882-02


Ultimate
ASTM D-
psi

5220
4600
5830


Tensile MD
882-02


% Elongation
ASTM D-


800
840
750


CD
882-02


% Elongation
ASTM D-


630
715
690


MD
882-02


Yield Strength
ASTM D-
psi
3350-
3080
3270
3170


CD
882-02

4250


Yield Strength
ASTM D-
psi
2750-
3065
2950
2980


MD
882-02

3450


Secant
ASTM D-
psi

102600
88200
97200


Modulus 1%
882-02


CD


Secant
ASTM D-
psi

82600
72000
77500


Modulus 2%
882-02


CD


Secant
ASTM D-
psi

82700
76600
82800


Modulus 1%
882-02


MD


Secant
ASTM D-
psi

66400
63400
64400


Modulus 2%
882-02


MD








Claims
  • 1. A film comprising at least one component formed from a composition, comprising a blend, wherein said blend comprises a high molecular weight ethylene-based interpolymer and a low molecular weight ethylene-based interpolymer, and wherein the high molecular weight ethylene-based interpolymer is a heterogeneously branched linear or a homogeneously branched linear ethylene-based interpolymer, and has a density from 0.922 g/cc to 0.929 g/cc, and a high load melt index (I21) from 0.2 g/10 min to 1.0 g/10 min, andwherein the low molecular weight ethylene-based interpolymer is heterogeneously branched linear or a homogeneously branched linear ethylene-based interpolymer, and has a density from 0.940 g/cc to 0.955 g/cc, and a melt index (I2) from 6 g/10 min to 50 g/10 min; andwherein the blend has a single peak in an ATREF profile eluting above 30° C., and has a coefficient of viscosity average molecular weight (CMv) less than −0.0032 in the log(calculated Mv) versus elution temperature, said CMv calculated in the range of elution temperatures from 70° C. to 90° C., and wherein Mv is the viscosity average molecular weight, andwherein the composition has an I21/I2 ratio from 30 to 80 and a density less than, or equal to, 0.945 g/cc.
  • 2. The film of claim 1, wherein the high molecular weight ethylene interpolymer has a density from 0.9229 g/cc to 0.9271 g/cc.
  • 3. The film of claim 1, wherein the CMv is less than −0.0036.
  • 4. The film of claim 1, wherein the blend is an in-situ blend.
  • 5. The film of claim 1, wherein the composition has a density from 0.930 g/cc to 0.945 g/cc.
  • 6. The film of claim 1, wherein the high molecular weight ethylene-based interpolymer is present in an amount from 45 to 55 weight percent, based on the sum weight of the high molecular weight ethylene-based interpolymer and the low molecular weight ethylene-based interpolymer.
  • 7. The film of claim 1, wherein the composition has a melt index, 12, from 0.05 g/10 min to 0.5 g/10 min.
  • 8. The film of claim 1, wherein the high molecular weight ethylene-based interpolymer is an ethylene/α-olefin interpolymer.
  • 9. The film of claim 1, wherein the low molecular weight ethylene-based interpolymer is an ethylene/α-olefin interpolymer.
  • 10. The film of claim 1, wherein the film is a multi-layered film.
  • 11. The film of claim 1, wherein the film is a single layered film.
  • 12. The film of claim 1, wherein the film has a thickness from 2 mils to 50 mils.
  • 13. The film of claim 1, wherein the film has an Elmendorf Tear Strength greater than, or equal to, 100 g/mil, in the machine direction.
  • 14. The film of claim 1, wherein the film has an Elmendorf Tear Strength greater than, or equal to, 220 g/mil, in the traverse direction.
  • 15. The film of claim 1, wherein the film has a Normalized Dart Impact (B scale) greater than, or equal to, 60 g.
  • 16. The film of claim 1, wherein the high molecular weight ethylene-based interpolymer is a heterogeneously branched linear ethylene-based interpolymer.
  • 17. The film of claim 1, wherein the low molecular weight ethylene-based interpolymer is a heterogeneously branched linear ethylene-based interpolymer.
  • 18. The film of claim 1, wherein weight ratio of the high molecular weight component to the low molecular weight component is from 55/45 to 45/55.
REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of U.S. Provisional Application No. 60/943,680, filed on Jun. 13, 2007, and U.S. Provisional Application No. 60/853,652, filed on Oct. 23, 2006; each application is fully incorporated herein by reference.

PCT Information
Filing Document Filing Date Country Kind 371c Date
PCT/US2007/081894 10/19/2007 WO 00 4/15/2010
Publishing Document Publishing Date Country Kind
WO2008/153586 12/18/2008 WO A
US Referenced Citations (5)
Number Name Date Kind
6248831 Maheshwari et al. Jun 2001 B1
6770341 Bohm et al. Aug 2004 B1
20040034169 Zhou et al. Feb 2004 A1
20040158001 Hamrock Aug 2004 A1
20040158011 Jain et al. Aug 2004 A1
Foreign Referenced Citations (15)
Number Date Country
0492656B1 Jul 1992 EP
WO 9612762 May 1996 WO
WO-9729152 Aug 1997 WO
WO-0001765 Jan 2000 WO
WO-0018814 Apr 2000 WO
WO-0040620 Jul 2000 WO
WO-0102480 Jan 2001 WO
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WO 2004025523 Mar 2004 WO
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WO-2008153586 Dec 2008 WO
Related Publications (1)
Number Date Country
20100203311 A1 Aug 2010 US
Provisional Applications (2)
Number Date Country
60943680 Jun 2007 US
60853652 Oct 2006 US