Tube bundle heat exchanger

Information

  • Patent Grant
  • 10914527
  • Patent Number
    10,914,527
  • Date Filed
    Wednesday, November 23, 2016
    7 years ago
  • Date Issued
    Tuesday, February 9, 2021
    3 years ago
Abstract
A tube bundle heat exchanger has tubes which are held at each side in tube plates or oval-tube collecting-tube plates and are connected to these in each case by means of a weld seam. The connection of the tubes to the inlet-side tube plate or oval-tube collecting-tube plate is formed in each case by means of a conical and/or trumpet-shaped transition piece. The cross section of the transition piece reduces as viewed in the gas flow direction in such a way that the inlet-side end, as viewed in the gas flow direction, of the transition piece is connected in a buttjoint to the tube plate or oval-tube collecting-tube plate. The inner and outer contours of the transition piece and of the welded connection region are formed without gaps and comers to the tube plate or oval tube collecting-tube plate and so as to be straight and/or with a radius, measured from the outer contour, of at least 5 mm.
Description
TECHNICAL FIELD

The invention relates to a tube bundle heat exchanger having tubes that are held at each side in tube plates or oval tube collecting tube plates and are connected to these in each case by means of a weld seam, for cooling, by means of a cooling medium surrounding the tubes, a hot gas flow that is directed through the tubes, exhibiting at least one gas inlet chamber, from which the hot gas flow is directed into the individual tubes and which is delimited at one side by the inlet-side tube plate or oval tube collecting tube plate, and at least one gas outlet chamber in which the gas flow directed through the tubes is collected and discharged and which is delimited on one side by the outlet-side tube plate or oval tube collecting tube plate.


BACKGROUND

As a rule, for cooling gases in many materials processing installations, such as, for example, gasification installations, thermal and catalytic splitting installations, steam reforming installations, etc., heat exchangers, in particular, tube bundle heat exchangers (coolers), are used, into which the gases—to be cooled flow through straight tubes and thereby give off the latent heat of the hot gas through the tube wall to the medium surrounding the tubes, in particular, the cooling medium. It is characteristic of such heat exchangers that the gases to be cooled are often under high pressure and at a high temperature and enter the straight tubes of the heat exchanger at high speed. As a result, at the tube inlet or the first section of the tube, a high heat flow density is achieved, which causes both a high temperature as well as high thermal stress in the tubes of the heat exchanger or in the tube plate—tube connection.


In state of the art heat exchangers, the tubes that conduct the gas are welded into the tube plates, whereby the weld seam between tube plate and tube is applied either at the outer or inner wall of the tube plate or inside the tube plate opening. For example, printed document DE 37 15 713 C2 exhibits a welded connection of the tube or tubes with the outer wall of the tube plate or the oval tube collecting tube plate.


The disadvantage of this known design consists in the fact that the gas-facing contour or surface of the transition from the tube to the tube plate or the oval tube collecting tube plate does not exhibit an exactly aerodynamic form. As a rule, the use of an inserted sleeve is undesirable for a number of different reasons, among them a narrowing of the gas-side cross section as well as an inadequate cooling of the sleeve. In addition, a gap can appear on the cooling medium side of the tube plates—tube connection, leading to water-side corrosion, or the tube plates—tube connection can exhibit a corner in which an unwanted stress concentration occurs.


Through document EP 1 154 143 A 1, a cooler has become known in whose heat exchanger tubes, which lie between an inlet-side tube plate and an outlet-side tube plate, an exhaust gas is cooled by cooling water. Through the cooling of the exhaust gas, a condensate that exhibits a corrosive component is created, which causes corrosion at the connection of the particular tube with the outlet-side tube plate.


As a result of this corrosion, a leak of the cooling water occurs at this connection, which leads to damage of the downstream machine. To prevent the leak, it is suggested that the connection of the particular tube with the outlet-side tube plate be designed in such a way that the tube is placed through the tube plate in a conical manner and the conical part of the tube is completely laser welded to the tube plate in order to achieve a deep-reaching welded connection.


SUMMARY

The task of the present invention consists in creating a tube bundle heat exchanger in which the disadvantages cited above can be avoided, and the transition from the tube plate or oval tube collecting tube plate to the tubes on the gas side exhibits a contour that is favorable to flow and no disturbing elements are present on the cooling medium side and the gas side.


The solution provides that the connection of the tubes with the inlet-side tube plate or oval header tube sheet is formed in each case by means of a conical and/or trumpet-shaped transition piece whose cross section reduces, as viewed in the gas flow direction, in such a way that the inlet-side end, as viewed in the gas flow direction, of the transition piece is connected in the manner of a butt joint to the tube plate or oval header tube sheet, and the inner and outer contours of the transition piece and of the welded connection region are formed without gaps and corners to the tube plate or oval header tube sheet, and so as to be straight and/or with a radius, measured from the outer contour, that is equal to or greater than 5 mm.


Through the solution according to the invention, a tube bundle heat exchanger is created that exhibits the following advantages:


By avoiding the protruding corners and gaps at the connecting location between the tubes and the tube plate or the oval tube collecting tube plate, first, turbulence of the gas and the cooling medium is prevented, and second, corrosion is eliminated,


The transition from the tube plate or the oval tube collecting tube plate to the tubes is designed aerodynamically, so that the entry of the gas into the tubes runs to the greatest extent turbulence-free, and temperature peaks in the inlet region can be reduced.


In an advantageous further development, the length Lu of the transition piece is at least 1.5 times the inside diameter di of the heat exchanger tube and/or the inside diameter Di of the transition piece at its inlet is at least 1.2 times the inside diameter di of the heat exchanger tube in order to achieve an optimized aerodynamic transition of the tube plate or the oval tube collecting tube plate to the particular heat exchanger tubes.


It is useful to mechanically widen the transition piece at the inlet-side end of the tube, as viewed in the gas flow direction. Through this measure, only one part—the tube—is fabricated, and the work process for the manufacture of the transition piece according to the invention can be simplified and shortened.


In an advantageous further development of the invention, the transition piece is formed from a separate tube part, and the outlet-side end, as viewed in the gas flow direction, of the transition piece is connected in the manner of a butt joint with the tube by means of weld seam. Through the use of a separate tube part, even transition pieces that are complicated in their form (for example, various differing transition radii) can be manufactured in a substantially simpler and less expensive way. In this further development of the invention, it is useful to form the inner and outer contours of the welded connection region between the transition piece and the tube without gaps and corners and so as to be straight and/or with a radius equal to or greater than 5 mm. Through this measure, an aerodynamic form is achieved at the inlet of the gas into the tube.


In an especially advantageous manner, the inner and outer contours of the transition piece and of the welded connection region to the tube plate or the oval tube collecting tube plate and to the tube are formed without gaps and corners, and so as to be straight and/or with a radius equal to or greater than 2 mm.


The tube part that is used as the transition piece is usefully formed as a forged piece.





BRIEF DESCRIPTION OF THE DRAWINGS

In the following, embodiments of the invention are explained in more detail with the aid of the drawing and the description.


The following are shown:



FIG. 1 is a longitudinal section through a tube bundle heat exchanger.



FIG. 2 is a detail section of the transition from the tube plate to the tube in accordance with detail “A” from FIG. 1.



FIG. 3 is an alternative design of FIG. 2.



FIG. 4 is an alternative design of FIG. 2.



FIG. 5 is a detail section of the transition of an oval tube collecting tube plate to a tube.





DETAILED DESCRIPTION


FIG. 1 shows a tube bundle heat exchanger 1 represented schematically in longitudinal section. Tube bundle heat exchangers 1 of this type are needed in many material processing installations, such as, for example, gasification installations, thermal and catalytic splitting installations, steam reforming installations, etc., in which a process gas, an exhaust gas or something similar is produced. As a rule, the tube bundle heat exchanger 1 is used for cooling the hot gas 18 mentioned above, which is introduced into the gas inlet chamber 8 of the heat exchanger 1 via a line, not shown, and is directed from here through a multiplicity of straight tubes 2, subsequently collected in the gas outlet chamber 9 of the heat exchanger 1 and discharged from the heat exchanger 1 by means of a line, not shown. In that regard, the tubes 2, by means of which an indirect heat exchange with a cooling medium 19 surrounding the tubes 2 takes place, are arranged at a distance from each other between two tube plates 3, 4 or oval tube collecting tube plates 5, 6 and are connected with the latter in fixed and gas-tight usually welded fashion.


In order to keep the thermal stresses taking place at the entry of the hot gas 18 from the gas inlet chamber 8 into the particular heat exchanger tubes 2 at the inlet-side, as viewed in the gas flow direction, tube plates 3, 5 and the inlet-side ends 16 of the tubes 2 as small as possible, according to the invention the connection of the tubes 2 with the inlet-side tube plate 3 (see FIGS. 2 through 4) or oval tube collecting tube plate 5 (see FIG. 5) is formed in each case by means of a conical and/or trumpet-shaped transition piece 10 whose cross section decreases as viewed in the gas flow direction (see arrow). Moreover, the inlet-side end 16, as viewed in the gas flow direction, of the transition piece 10 is connected in the manner of a butt joint to the tube plate 3 or oval tube collecting tube plate 5, and the inner and outer contours 11, 12 of the transition piece 10 and of the welded connection region 13 are formed without gaps and corners to the tube plate 3 or oval tube collecting tube plate 5, and so as to be straight and/or with a radius, measured from the outer contour 12, of at least 5 mm.


This means that the inventive design of the transition from the tube plate 3 or the oval tube collecting tube plate 5 to the tube 2 creates an aerodynamic contour 11, 12 on both the gas-contacted and cooling medium-contacted side of the tube 2, of the transition piece 10 and of the tube plate 3 or oval tube collecting tube plate 5, which does not exhibit a gap, a corner or an angular transition anywhere. This means that according to the invention, all of the transitions, including that of the welded transition region 13 to the inner or outer contour 11, 12, are either straight or flat, and/or are designed with a radius.


According to FIGS. 2 and 5, the transition piece 10 is the widened, e.g. mechanically, from the tube 2 at diameter di transitioning to diameter Di at the inlet end 16 of tube 2. In this design, only weld seam 7 is needed between the tube 2 and the tube plate 3 or 5, which forms the welded connection region 13 between the tube 2 and the tube plate 3, 5. FIGS. 3 and 4 show a transition piece 10 that consists of a separate tube part 15 and is as a rule easier to manufacture, since the tube part 15 is significantly shorter than the complete tube 2 and is thus easier to process as well. For the head-side connection of the outlet-side end 17, as viewed in the gas flow direction, of the tube part 15, an additional weld seam 22 is needed, which forms the welded connection region 14 between the tube 2 and the tube part 15. This welded connection region 14 is advantageously made either straight or flat and/or with a radius both on the inside as well as on the outside contour 11, 12, i.e., the region 14 is made without corners and gaps.


The transition pieces 10 according to FIGS. 2 through 5 exhibit on their inlet-side end 16, relative to the outer contour 12 of the transition pieces 10, a radius R1 of 5 mm, for example. According to FIGS. 2, 3 and 5, adjoining that is an additional radius R2 of 60 mm, for example. By contrast, in the case of the transition piece 10 according to FIG. 4, adjoining the first radius is a conical contraction (e.g., conical transition piece 10) having an inlet-side transition segment T1 with a first inner contour and a first outer contour and an outlet-side transition segment T2 with a second inner contour and a second outer contour. The first outer contour having a radius of curvature of 20 mm, for example, at the inlet-side transition segment T1. The second outer contour having a radius of curvature of at least 5 mm at the outlet-side transition segment T2. As shown in FIG. 4 the tubes 2 include a conical transition piece 10 expanding outwardly from a first end 10A to a second end 10B thereof. The first end 10A extends from the inlet-side transition segment T1 of a respective one of the plurality of tubes 15. The second end 10B terminates at the outlet-side transition segment T2 of the respective one the tubes 2 at the inlet end 16 at the respective opening of the inlet-side tube plate 3.


The inside contour 11 of the transition pieces 10 according to FIGS. 2 and 5 then exhibits corresponding radii that are greater by the wall thickness s of the transition piece 10. If the wall thickness t of the tube plate 3, 5 does not correspond to the wall thickness s of the tube 2, then according to the invention the transition between the two wall thickness s and t within the welded connection region 13 is designed according to the invention either straight or flat and/or with a radius. A wall thickness t of the tube plates 3, 5 that differs from the wall thickness s of the tube 2 can be compensated according to FIGS. 3 and 4 with a transition piece 10 designed. as a tube part 15, in that the particular wall thickness at the tube ends of the tube part 15 are adjusted to the wall thicknesses t and s of the tube plate 3, 5 as well as of the tube 2. This means that, viewed in the gas flow direction, inside the tube piece 15 the wall thickness t continuously decreases or increases to the wall thickness s. In that regard, the tube part 15 can advantageously be designed as a forged part.


The length LO of the transition piece 10 is advantageously 1.5 times the inside diameter di of the tube 2 and the inside diameter Di of the transition piece 10 directly at the entry into the transition piece 10 is advantageously 1.2 times the inside diameter di of the tube 2.


By way of example, FIG. 4 shows in place of the trumpet-shaped transition piece 10 a conical transition piece 10, which is also formed from a separate tube part 15. Here again, the tube part 15 is connected with the tube plate 3 and the tube 2 by two weld seams 7, 22.



FIG. 5 shows a tube bundle heat exchanger 1 with double tubes 2, 21 in which the cooling medium 19 circulates in the annular cross section between the inner tube 2 and the outer tube 21. Because of the outer tubes 21 that carry the cooling medium 19, the heat exchanger outer jacket 23, which is shown in FIG. 1 and which would otherwise be required, can be dispensed with. While in the case of the heat exchanger 1 shown in FIG. 1, the cooling medium 19 is fed to and discharged from the space inside the outer jacket 23 and the tube plates 3, 5 and 4, 6, according to FIG. 5 the cooling medium 19 is fed and discharged by means of oval tube collector 20. In this case, the connection of the transition piece 10 according to the invention takes place with the oval tube collecting tube plate 5.


Water that is partially or completely vaporized by the addition of heat can be used as the cooling medium 19.


LIST OF REFERENCE SYMBOLS




  • 1 Tube bundle heat exchanger


  • 2 Tube


  • 3 Tube plate, inlet side.


  • 4 Tube plate, outlet side


  • 5 Oval tube collecting tube plate, inlet side


  • 6 Oval tube collecting tube plate, outlet side


  • 7 Weld seam


  • 8 Gas inlet chamber


  • 9 Gas outlet chamber


  • 10 Transition piece


  • 10A outlet-side end


  • 10B inlet-side end

  • T1 inlet-side transition segment

  • T2 outlet-side transition segment


  • 11 Inside contour


  • 12 Outside contour


  • 13 Welded connection region


  • 14 Welded connection region


  • 15 Tube part


  • 16 Inlet-side end of the transition piece or of the tube


  • 17 Outlet-side end of the transition piece or of the tube


  • 18 Gas


  • 19 Cooling medium


  • 20 Oval tube collector


  • 21 Outer tube


  • 22 Weld seam


  • 23 Jacket


Claims
  • 1. A tube bundle heat exchanger comprising: a gas inlet chamber adapted to receive a gas into the heat exchanger;a gas outlet chamber adapted to emit the gas from the heat exchanger;an inlet-side tube plate disposed proximate to the gas inlet chamber, the inlet-side tube plate having a substantially flat axially outward facing surface, the inlet-side tube plate having a plurality of inlet-openings that are coplanar with the axially outward facing surface;an outlet-side tube plate disposed proximate to the gas outlet chamber, the outlet-side tube plate having a plurality of outlet-openings; anda plurality of tubes, each of the plurality of tubes having an inlet end with a first circular cross sectional flow area having a first inside diameter and each of the plurality of tubes having an outlet end, each of the inlet-openings of the inlet-side tube plate being circular;wherein the outlet end of each of the plurality of tubes is welded to a respective outlet-opening of the outlet-side tube plate;a transition piece attached to at least one of the plurality of tubes, the transition piece comprising; (i) a tubular segment having a first circular cross sectional flow opening and the first inside diameter, the tubular segment extending along a longitudinal axis of the transition piece, the tubular segment having an outlet-side end at the first cross sectional flow opening, the outlet-side end being welded to the inlet end of a respective one of the plurality of tubes;(ii) an arcuate outlet-side transition segment extending from the tubular segment towards a respective one of the inlet-openings of the inlet-side tube plate, the outlet-side transition segment having an axially extending arcuate outlet-side inside surface and an axially extending arcuate outlet-side exterior surface, the axially extending arcuate outlet-side exterior surface having an outlet-side radius of curvature;(iii) a conical transition segment extending from the arcuate outlet-side transition segment and expanding symmetrically away from the longitudinal axis and outwardly toward a respective one of the inlet-openings of the inlet-side tube plate;(iv) an inlet-side transition segment having an axially extending arcuate inlet-side inside surface and an axially extending arcuate inlet-side exterior surface, the axially extending arcuate inlet-side exterior surface having an inlet-side radius of curvature, the arcuate inlet-side transition segment extending a length from the conical transition segment toward and welded to a respective one of the inlet-openings and the arcuate inlet-side transition segment having circular cross sections entirely along the length thereof and having a second circular cross sectional flow opening that is substantially coplanar with the axially outward facing surface the inlet-side tube plate and the second circular cross sectional flow opening having a second inside diameter that is greater than the first inside diameter of the first cross sectional flow opening; andwherein each of the plurality of tubes and the transition piece provide fluid communication of the gas between the gas inlet chamber and the gas outlet chamber,wherein the axially extending arcuate inlet-side inside surface and the axially extending arcuate inlet-side exterior surface are formed without gaps or corners to the inlet-side tube plate, andfurther wherein the outlet-side radius of curvature is 20 mm and the inlet-side radius of curvature is 5 mm.
  • 2. The tube bundle heat exchanger of claim 1, wherein the arcuate outlet-side transition segment further comprises an outlet-side inner contour.
  • 3. The tube bundle heat exchanger of claim 1, wherein the inlet-side inner contour and the inlet-side outer contour being formed without gaps or corners to the inlet-side tube plate.
  • 4. The tube bundle heat exchanger of claim 1, wherein the inlet-side transition segment is welded to a respective one of the inlet-openings without gaps and corners.
  • 5. The tube bundle heat exchanger of claim 1, wherein the transition piece has a length that is 1.5 times the second inside diameter.
  • 6. The tube bundle heat exchanger of claim 1, wherein the second inside diameter is at least 1.2 times the first inside diameter.
  • 7. A tube bundle heat exchanger comprising: a gas inlet chamber adapted to receive a gas into the heat exchanger;a gas outlet chamber adapted to emit the gas from the heat exchanger;an inlet-side tube plate disposed proximate to the gas inlet chamber, the inlet-side tube plate having a substantially flat axially outward facing surface, the inlet-side tube plate having a plurality of inlet-openings that are coplanar with the axially outward facing surface;an outlet-side tube plate disposed proximate to the gas outlet chamber, the outlet-side tube plate having a plurality of outlet-openings; anda plurality of tubes, each of the plurality of tubes having an inlet end with a first circular cross sectional flow opening having a first inside diameter and each of the plurality of tubes having an outlet end, each of the inlet-openings of the inlet-side tube plate being circular;wherein the outlet end of each of the plurality of tubes is welded to a respective outlet-opening of the outlet-side tube plate;a transition piece attached to at least one of the plurality of tubes, the transition piece comprising:(i) an arcuate outlet-side transition segment welded to the inlet end of a respective one of the plurality of tubes and extending toward a respective one of the inlet-openings of the inlet-side tube plate, the arcuate outlet-side transition segment having an axially extending arcuate outlet-side inside surface and an axially extending arcuate outlet-side exterior surface, the axially extending arcuate outlet-side exterior surface having an outlet-side radius of curvature;(ii) a conical transition segment extending from the outlet-side transition segment and toward a respective one of the inlet-openings of the inlet-side tube plate;(iii) an inlet-side transition segment having an axially extending arcuate inlet-side inside surface and an axially extending arcuate inlet-side exterior surface, the axially extending inlet-side exterior surface having an inlet-side radius of curvature, the arcuate inlet-side transition segment extending a length from the conical transition segment toward and welded to a respective one of the inlet-openings and the arcuate inlet-side transition segment having circular cross sections entirely along the length thereof and having a second circular cross sectional flow opening that is substantially coplanar with the axially outward facing surface of the inlet-side tube plate and the second circular cross sectional flow opening having a second inside diameter that is greater than the first inside diameter of the first cross sectional flow area, and outlet-side radius of curvature being greater than the first inlet-side radius of curvature; andwherein each of the plurality of tubes and the transition piece provide fluid communication of the gas between the gas inlet chamber and the gas outlet chamber,wherein the axially extending arcuate inlet-side inside surface and the axially extending arcuate inlet-side exterior surface are formed without gaps or corners to the inlet-side tube plate, andfurther wherein the outlet-side radius of curvature is 20 mm and the inlet-side radius of curvature is 5 mm.
  • 8. A method for using the tube bundle heat exchanger according to claim 7, comprising: introducing the gas to the conical transition segment from the inlet-side tube plate.
  • 9. The tube bundle heat exchanger of claim 7, wherein the inlet-side transition segment is welded to a respective one of the inlet-openings without gaps and corners.
Priority Claims (1)
Number Date Country Kind
10 2006 003 317 Jan 2006 DE national
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation application of co-pending U.S. patent application Ser. No. 12/087,444 filed Jul. 3, 2008, entitled “Tube Bundle Heat Exchanger,” that is a U.S. national stage application of International Application No. PCT/DE2007/000089, filed Jan. 19, 2007.

US Referenced Citations (167)
Number Name Date Kind
682607 Eck Sep 1901 A
1429149 Lawrence Sep 1922 A
1450351 Beran Apr 1923 A
1875188 Beran Apr 1923 A
1477209 Cowan Dec 1923 A
1524280 Bancel Jan 1925 A
1894956 Kerr Jan 1933 A
1915742 Mautsch Jun 1933 A
1987798 Ruppricht Jan 1935 A
2023965 Lysholm Dec 1935 A
2042017 Orchard May 1936 A
2102936 Bailey Dec 1937 A
2160677 Romanoff May 1939 A
2313081 Ljungstrom Mar 1943 A
2438851 Gates Mar 1948 A
2596642 Boestad May 1952 A
2782009 Rippingille Feb 1957 A
2796157 Ginsburg Jun 1957 A
2940736 Odman Jun 1960 A
2983486 Rosenberg May 1961 A
3019160 Slezak et al. Jan 1962 A
3111982 Ulbricht Nov 1963 A
3158527 Faccin et al. Nov 1964 A
3183963 Mondt May 1965 A
3216494 Goodman Nov 1965 A
3240266 Corbet et al. Mar 1966 A
3260511 Greer Jul 1966 A
3262490 Olson Jul 1966 A
3317222 Maretzo May 1967 A
3372743 Pall et al. Mar 1968 A
3373798 Brummett Mar 1968 A
3415502 Munters Dec 1968 A
3452814 Malewicz Jul 1969 A
3490523 Esmond Jan 1970 A
3523058 Shick Aug 1970 A
3532157 Hubble Oct 1970 A
3540529 Umino et al. Nov 1970 A
3542635 Parker Nov 1970 A
3574103 Latkin Apr 1971 A
3674620 McCarthy et al. Jul 1972 A
3726408 Gewiss Apr 1973 A
3759323 Dawson et al. Sep 1973 A
3825412 Mullender Jul 1974 A
3830684 Hamon Aug 1974 A
3887664 Regehr Jun 1975 A
RE28534 Arne Aug 1975 E
3901309 Thebert Aug 1975 A
3940966 Deane Mar 1976 A
3941185 Henning Mar 1976 A
3952077 Wigley Apr 1976 A
3963810 Holmberg et al. Jun 1976 A
4034135 Passmore Jul 1977 A
4049855 Cogan Sep 1977 A
4061183 Davis Dec 1977 A
4098722 Cairns et al. Jul 1978 A
4106558 Neveux Aug 1978 A
4125149 Kritzler et al. Nov 1978 A
4144369 Wass Mar 1979 A
4182402 Adrian Jan 1980 A
4202449 Bendt May 1980 A
4228847 Lindahl Oct 1980 A
4296050 Meier Oct 1981 A
4320073 Bugler Mar 1982 A
4337287 Falkenberg Jun 1982 A
4343355 Goloff et al. Aug 1982 A
4344899 Monjoie Aug 1982 A
4361426 Carter et al. Nov 1982 A
4363222 Cain Dec 1982 A
4374542 Bradley Feb 1983 A
4396058 Kurschner et al. Aug 1983 A
4409274 Chaplin et al. Oct 1983 A
4423772 Dahlgren Jan 1984 A
4449573 Pettersson et al. May 1984 A
4472473 Davis et al. Sep 1984 A
4501318 Hebrank Feb 1985 A
4512389 Goetschius Apr 1985 A
4518544 Carter et al. May 1985 A
4553458 Schoonover Nov 1985 A
4605996 Payne Aug 1986 A
4633936 Nilsson Jan 1987 A
4668443 Rye May 1987 A
4676934 Seah Jun 1987 A
4689261 Ahnstrom Aug 1987 A
4744410 Groves May 1988 A
4750553 Pohl et al. Jun 1988 A
4769968 Davis et al. Sep 1988 A
4791773 Taylor Dec 1988 A
4842920 Banai et al. Jun 1989 A
4847019 McNab Jul 1989 A
4857370 Overbergh et al. Aug 1989 A
4858684 Brucher et al. Aug 1989 A
4862666 Kero Sep 1989 A
4876134 Saitoh et al. Oct 1989 A
4906510 Todor, Jr. et al. Mar 1990 A
4915165 Dahlgren et al. Apr 1990 A
4930569 Harder Jun 1990 A
4950430 Chen et al. Aug 1990 A
4953629 Karlsson et al. Sep 1990 A
4974656 Judkins Dec 1990 A
4981732 Hoberman Jan 1991 A
5031692 Kehrer Jul 1991 A
5085268 Nilsson Mar 1992 A
5101892 Takeuchi et al. Apr 1992 A
5150596 Hunt et al. Sep 1992 A
5308677 Renna May 1994 A
5314006 Kaastra et al. May 1994 A
5314738 Ichikawa May 1994 A
5318102 Spokoyny et al. Jun 1994 A
5333482 Dunlap et al. Aug 1994 A
5380579 Bianchi Jan 1995 A
5413741 Buchholz et al. May 1995 A
5413872 Faigle May 1995 A
5441793 Siiess Aug 1995 A
5489463 Paulson Feb 1996 A
5544703 Joel et al. Aug 1996 A
H001621 Ray Dec 1996 H
5598930 Leone et al. Feb 1997 A
5600928 Hess et al. Feb 1997 A
5605655 Ishihara et al. Feb 1997 A
5609942 Ray Mar 1997 A
5647741 Bunya et al. Jul 1997 A
5667875 Usui Sep 1997 A
5747140 Heerklotz May 1998 A
5792539 Hunter Aug 1998 A
5803158 Harder et al. Sep 1998 A
5836379 Counterman Nov 1998 A
5899261 Brzytwa et al. May 1999 A
5979050 Counterman et al. Nov 1999 A
5983985 Counterman et al. Nov 1999 A
6019160 Chen Feb 2000 A
6145582 Bolle et al. Nov 2000 A
6212907 Billingham et al. Apr 2001 B1
6251499 Lehman et al. Jun 2001 B1
6263570 Cazacu Jul 2001 B1
6280824 Insley et al. Aug 2001 B1
6280856 Anderson et al. Aug 2001 B1
6478290 Ender et al. Nov 2002 B1
6497130 Nilsson Dec 2002 B2
6516871 Brown et al. Feb 2003 B1
6544628 Aull et al. Apr 2003 B1
6660402 Tanabe Dec 2003 B2
6730008 Liang May 2004 B1
6764532 Cheng Jul 2004 B1
7044206 Sabin et al. May 2006 B2
7117928 Chen Oct 2006 B2
7347351 Slattery May 2008 B2
7555891 Muller et al. Jul 2009 B2
7654067 Wattron Feb 2010 B2
7938627 Muller May 2011 B2
8296946 Wieres et al. Oct 2012 B2
8323778 Webb et al. Dec 2012 B2
9200853 O'Boyle et al. Dec 2015 B2
9534850 Jekerle Jan 2017 B2
20020043362 Wilson Apr 2002 A1
20030024697 Matsuzaki Feb 2003 A1
20030178173 Harting et al. Sep 2003 A1
20050274012 Hodgson et al. Dec 2005 A1
20070017664 Beamer et al. Jan 2007 A1
20090065185 Jekerle Mar 2009 A1
20100218927 Cooper et al. Sep 2010 A1
20100258284 Krantz Oct 2010 A1
20100282437 Birmingham et al. Nov 2010 A1
20120305217 Cowburn et al. Dec 2012 A1
20130327513 Franz et al. Dec 2013 A1
20140054003 O'Boyle et al. Feb 2014 A1
20140090822 Seeblad Apr 2014 A1
20150144293 Seebald May 2015 A1
Foreign Referenced Citations (37)
Number Date Country
1061653 Sep 1979 CA
2759895 Nov 2010 CA
101210780 Jul 2008 CN
0150913 Aug 1985 EP
0805331 Nov 1997 EP
0945195 Sep 1999 EP
1154143 Nov 2001 EP
1884732 Feb 2008 EP
2427712 Nov 2010 EP
775271 Dec 1934 FR
1219505 May 1960 FR
177780 Feb 1923 GB
992413 May 1965 GB
1339542 Dec 1973 GB
1567239 May 1980 GB
83112 Sep 1929 JP
26-006787 Oct 1951 JP
S52-000746 Jan 1977 JP
S54-085547 Jun 1979 JP
S56-075590 Jun 1981 JP
S57-154874 Sep 1982 JP
93590 Jun 1987 JP
158996 Jul 1987 JP
01-273996 Nov 1989 JP
08-101000 Apr 1996 JP
09-280764 Oct 1997 JP
10-328861 Dec 1998 JP
11-294986 Oct 1999 JP
2001-516866 Oct 2001 JP
2003-200223 Jul 2003 JP
2004-093036 Mar 2004 JP
100417321 Feb 2004 KR
1020080063271 Jan 2013 KR
99014543 Mar 1999 WO
2007012874 Feb 2007 WO
2010129092 Nov 2010 WO
2012000767 Jan 2012 WO
Non-Patent Literature Citations (1)
Entry
English Translation of Reason for Refusal for Japanese Patent Application No. 2012-509814, dated Feb. 24, 2014, pp. 1-7.
Related Publications (1)
Number Date Country
20170074593 A1 Mar 2017 US
Continuations (1)
Number Date Country
Parent 12087444 US
Child 15359995 US