(1) Field
The present disclosure relates generally to spoolable tubing, and more particularly to spoolable tubing or pipes capable of operating in a pressure range that may be considered below the pressure ranges generally suited to fiber reinforced composite or metallic spoolable pipe, but above the pressure ranges generally suited to unreinforced polymeric pipes.
(2) Description of Relevant Art
Spoolable tubing, or tubing capable of being spooled upon a reel, is commonly used in numerous oil well operations, although other applications exist. For example, oil well operations include running wire line cable down hole with well tools, working over wells by delivering various chemicals down hole, and performing operations on the interior surface of the drill hole. The tubes are spoolable so that a tube can be used with one well, and then transported on a reel to another well at a different location. Steel coiled tubing is typically capable of being spooled because the steel used in the product exhibits high ductility (i.e., the ability to plastically deform). Unfortunately, the repeated spooling and use of steel coiled tubing causes fatigue damage that can cause the steel coiled tubing to fracture and fail, often without notice. The hazards of operating steel coiled tubing, i.e., risk to personnel and high economic cost resulting from down-time needed to retrieve the broken tubing sections, forces steel coiled tubing to be retired after a relatively few number of trips into a well.
Steel coiled tubing has also proven to be subject to expansion after repeated uses. Tube expansion results in reduced wall thickness with the associated reduction in the pressure carrying capability of the steel coiled tubing. Steel coiled tubing known in the art is typically limited to an internal pressure up to about 5,000 psi. Accordingly, higher pressure and continuous flexing typically reduces the steel tube's integrity and service life.
For example, the present accepted industry standard for steel coiled tube is an A-606 type 4 modified HSLA steel with yield strengths ranging from 70 ksi to 80 ksi. The HSLA steel tubing typically undergoes bending, during the deployment and retrieval of the tubing, over radii significantly less than the minimum bending radii needed for the material to remain in an elastic state. The repeated bending of steel coiled tubing into and out of plastic deformation induces irreparable damage to the steel tube body leading to low-cycle fatigue failure.
Additionally, when steel coiled tubing is exposed to high internal pressures and bending loads, the isotropic steel is subjected to high triaxial stresses imposed by the added pressure and bending loads. The high triaxial stresses result in significant plastic deformation of the tube and diametral growth of the tube body, commonly referred to as “ballooning”. When the steel coiled tube experiences ballooning, the average wall thickness of the tube is reduced, and often causes a bursting of the steel tube in the area of decreased thickness.
Steel coiled tubes also experience thinning of the tube walls due to the corrosive effect of materials used in the process of working over the well and due to materials located on the inner surface of the well bore. The thinning resulting from corrosive effects of various materials causes a decrease in the pressure and the tensile load rating of the steel coiled tubing.
Spoolable tubing can also be installed in permanent applications such as in transport of oil and gas and produced materials from wells, or injection of materials into wellbores. Typically in these applications the spoolable pipe is buried, but it can also be installed on surface. Spoolable pipe can also be installed vertically in wellbores in permanent applications including production tubing, casing, or other conduits from surface.
When the ends of a tube are subjected to opposing forces, the tube is said to be under tension. The tensile stress at any particular cross-section of the tube is defined as the ratio of the force exerted on that section by opposing forces to the cross-sectional area of the tube. The stress is called a tensile stress, meaning that each portion pulls on the other.
With further reference to a tube subjected to opposing forces, the term strain refers to the relative change in dimensions or shape of the tube that is subjected to stress. For instance, when a tube is subjected to opposing forces, a tube whose natural length is L0 will elongate to a length L1=L0+ΔL, where ΔL is the change in the length of the tube caused by opposing forces. The tensile strain of the tube is then defined as the ratio of ΔL to L0, i.e., the ratio of the increase in length to the natural length.
The stress required to produce a given strain depends on the nature of the material under stress. The ratio of stress to strain, or the stress per unit strain, is called an elastic modulus. The larger the elastic modulus, the greater the stress needed for a given strain.
For an elastomeric type material, such as used in tubes, the elongation at break may be high (typically greater than 400 percent) and the stress-strain response may be highly nonlinear. Therefore, it is common practice to define a modulus of elasticity corresponding to a specified elongation. The modulus for an elastomeric material corresponding to 200 percent elongation typically ranges form 300 psi to 2000 psi. In comparison, the modulus of elasticity for typical plastic matrix material used in a composite tube is from 100,000 psi to 500,000 psi or greater, with representative strains to failure of from 2 percent to 10 percent. This large difference in modulus of elasticity and strain to failure between rubber and plastics and thus between tubes and composite tubes may permit a tube to be easily collapsed to an essentially flat condition under relatively low external pressure. This large difference may also eliminate the spoolable pipe's capability to carry high axial tension or compression loads while the higher modulus characteristic of the plastic matrix material used in a composite tube is sufficiently stiff to transfer loads into the fibers and thus resist high external pressure and axial tension and compression without collapse.
The procedure to construct a composite tube to resist high external pressure and compressive loads involves using complex composite mechanics engineering principles to ensure that the tube has sufficient strength. Such a composite tube is presented in U.S. Pat. Nos. 5,921,285, 6,016,845, 6,148,866, 6,286,558, 6,357,485, and 6,604,550 the entireties of which are incorporated herein by reference in their entireties. There are some applications in which the high external pressures for which such composite pipes are desirable, may not be present, and thus, other types of reinforced spoolable pipe may be preferable.
Disclosed is a spoolable pipe having a wall that includes an internal pressure barrier or liner formed about a longitudinal axis, and at least one reinforcing layer enclosing the internal pressure barrier, where the reinforcing layer(s) includes fibers having at least a partial helical orientation relative to the longitudinal axis.
Also disclosed is a spoolable tube that comprises an internal pressure barrier formed about a longitudinal axis; at least one reinforcing layer enclosing the internal pressure barrier, where the at least one reinforcing layer comprises at least two plies of fibers having at least a partial helical orientation relative to the longitudinal axis and whereat least one abrasion resistant layer is disposed between the at least two plies of fibers, the spoolable pipe also including an external layer enclosing the at least one reinforcing layer. The spoolable pipe of this disclosure can also include a reinforcing layer that includes at least two plies, at least four plies, or even at least eight plies of fibers that have about an equal but opposite helical orientation relative to the longitudinal axis. In certain embodiments, at least one abrasion layer is disposed between at least two plies, or for example, between each of the plies. In other embodiments, the plies may be counterwound unidirectional plies. In other embodiments, the fibers or plies may be axially oriented. The reinforcing layers may further include a coating, in some embodiments.
The internal pressure barriers of the disclosed spoolable tubes may carry at least twenty-five percent of the axial load along the longitudinal axis at a termination, or at least fifty percent of an axial load. Reinforcing layers of a spoolable tube may include glass, for example, e-glass, e-cr glass, Advantex®, and/or aramid, carbon, minerals, for example, basalt fibers, ceramic, metal or polymer.
This disclosure also provides for a spoolable pipe comprising an internal pressure barrier formed about a longitudinal axis, at least one reinforcing layer enclosing the internal pressure barrier, the at least one reinforcing layer including fibers having at least a partial helical orientation relative to the longitudinal axis, and, at least one external layer enclosing the at least one reinforcing layer and having a permeability at least five times greater, or at least ten times greater than the permeability of the internal pressure barrier.
The spoolable pipes disclosed herein may include a perforated or discontinuous external layer. The external layer may include a plurality of perforations. In other embodiments, the spoolable pipes disclosed herein may include one or more energy conductors.
Also disclosed herein is a spoolable pipe, comprising an internal pressure barrier formed about a longitudinal axis, at least one reinforcing layer enclosing the internal pressure barrier, the at least one reinforcing layer including fibers having at least a partial helical orientation relative to the longitudinal axis, the at least one reinforcing layer including a coating; and at least one external layer enclosing the at least one reinforcing layer. Such coatings can include silane compounds, sizing treatment, abrasion resistant compositions and water resistant compositions.
The spoolable pipes disclosed may also include a means for venting gasses or liquids. A spoolable pipe may include a fitting or coupling, for example, that interfaces with the internal barrier and/or the external layer.
Other objects and advantages will become apparent hereinafter in view of the specification and drawings.
To provide an overall understanding, certain illustrative embodiments will now be described; however, it will be understood by one of ordinary skill in the art that the systems and methods described herein can be adapted and modified to provide systems and methods for other suitable applications and that other additions and modifications can be made without departing from the scope of the systems and methods described herein.
Unless otherwise specified, the illustrated embodiments can be understood as providing exemplary features of varying detail of certain embodiments, and therefore, unless otherwise specified, features, components, modules, and/or aspects of the illustrations can be otherwise combined, separated, interchanged, and/or rearranged without departing from the disclosed systems or methods. Additionally, the shapes and sizes of components are also exemplary and unless otherwise specified, can be altered without affecting the scope of the disclosed and exemplary systems or methods of the present disclosure.
Disclosed is a spoolable tube that provides a path for conducting fluids (i.e., liquids and gases) along the length of the spoolable tube. For example, the spoolable tube can transmit fluids down a well hole for operations upon the interior surfaces of the well hole, the spoolable tube can transmit fluids or gases to hydraulic or pneumatic machines operably coupled to the spoolable tube, and/or the spoolable tube can be used to transmit fluids on surface from well holes to transmission or distribution pipelines. Accordingly, the spoolable tube can provide a conduit for powering and controlling hydraulic and/or pneumatic machines, and/or act as a conduit for fluids, for example gases or liquids.
The internal pressure barrier 12, otherwise referred to as a liner, can serve as a pressure containment member to resist leakage of internal fluids from within the spoolable tube 10. In some embodiments, the internal pressure barrier 12 can include a polymer, a thermoset plastic, a thermoplastic, an elastomer, a rubber, a co-polymer, and/or a composite. The composite can include a filled polymer and a nano-composite, a polymer/metallic composite, and/or a metal (e.g., steel, copper, and/or stainless steel). Accordingly, an internal pressure barrier 12 can include one or more of a high density polyethylene (HDPE), a cross-linked polyethylene (PEX), a polyvinylidene fluoride (PVDF), a polyamide, polyethylene terphthalate, polyphenylene sulfide and/or a polypropylene. In one embodiment, the internal pressure barrier 12 includes a modulus of elasticity greater than about approximately 50,000 psi, and/or a strength greater than about approximately 1,000 psi. In some embodiments, the internal pressure barrier 12 can carry at least fifteen percent of the axial load along the longitudinal axis, at least twenty-five percent of the axial load along the longitudinal axis, or at least thirty percent of the axial load along the longitudinal axis at a termination, while in some embodiments, the internal pressure barrier 12 can carry at least fifty percent of the axial load along the longitudinal axis at a termination. Axial load may be determined at the ends of a tube. For example, at the ends, or a termination, of a tube, there may be a tensile (e.g. axial) load equal to the internal pressure multiplied by the area of the pipe.
Referring back to
Exemplary fibers include but are not limited to graphite, KEVLAR, fiberglass, boron, polyester fibers, polymer fibers, mineral based fibers such as basalt fibers, and aramid. For example, fibers can include glass fibers that comprise e-cr glass, Advantex®, s-glass, d-glass, or a corrosion resistant glass.
The reinforcing layer(s) 14 can be formed of a number of plies of fibers, each ply including fibers. In one embodiment, the reinforcing layer(s) 14 can include two plies, which can optionally be counterwound unidirectional plies. The reinforcing layer(s) can include two plies, which can optionally be wound in about equal but opposite helical directions. The reinforcing layer(s) 14 can include four, eight, or more plies of fibers, each ply independently wound in a helical orientation relative to the longitudinal axis. Plies may have a different helical orientation with respect to another ply, or may have the same helical orientation. The reinforcing layer(s) 14 may include plies and/or fibers that have a partially and/or a substantially axial orientation. The reinforcing layer may include plies of fibers with an abrasion resistant material disposed between each ply, or optionally disposed between only certain plies. In some embodiments, an abrasion resistant layer is disposed between plies that have a different helical orientation.
The fibers can include structural fibers and flexible yarn components. The structural fibers can be formed of carbon, aramid, thermoplastic, and/or glass. The flexible yarn components, or braiding fibers, can be formed of either polyamide, polyester, aramid, thermoplastic, glass and/or ceramic. The fibers included in the reinforcing layer(s) 14 can be woven, braided, knitted, stitched, circumferentially (axially) wound, helically wound, and/or other textile form to provide an orientation as provided herein (e.g., in the exemplary embodiment, with an orientation between substantially about thirty degrees and substantially about seventy degrees relative to the longitudinal axis 17). The fibers can be biaxially or triaxially braided.
In one embodiment, the reinforcing layer(s) 14 includes fibers having a modulus of elasticity of greater than about 5,000,000 psi, and/or a strength greater than about 100,000 psi. In some embodiments, an adhesive can be used to bond the reinforcing layer(s) 14 to internal pressure barrier 12. In other embodiments, one or more reinforcing layers are substantially not bonded to one or more of other layers, such as the inner liner, internal pressure barriers, or external layer(s).
The fibers in each of the reinforcing layers 14A-C can be selected from the same or different material. For example, the first reinforcing layer 14A can comprise helically oriented glass fibers; second reinforcing layer 14B can comprise a ply having helically oriented glass fiber at the same angle, but at an opposite orientation of the first reinforcing layer 14A; and third reinforcing layer 14C can comprise plies of fibers having a clockwise and counter-clockwise helically oriented glass fibers. Further, the different reinforcing layers 14A-C can include different angles of helical orientation. For example, in one embodiment, the different layers can have angles of orientation between substantially about thirty degrees and substantially about seventy degrees, relative to the axis 17. Alternatively, the different layers can have angles of orientation between substantially about forty-six degrees and substantially about fifty-two degrees, relative to the axis 17. In some embodiments, the different layers 14A-C can have more than one fiber within a layer, such as carbon and glass, and/or carbon and aramid, and/or glass and aramid. Further, the different layers 14A-C may each comprise multiple plies, each independent ply having a different, or substantially the same, helical orientation with respect to other plies within a layer.
The fibers in each of plies 114A, B can be selected from the same or different material. For example, the ply 114A can comprise at least partially helically oriented glass fibers; second ply 114B can comprise a ply having at least partially helically oriented glass fiber at the same angle, but at an opposite orientation of the first ply 114A. Further, the plies 114A, B can include different angles of helical orientation. For example, in one embodiment, the different plies can have angles of orientation between substantially about thirty degrees and substantially about seventy degrees, relative to the axis 17. Alternatively, the different plies can have angles of orientation between substantially about forty-six degrees and substantially about fifty-two degrees, relative to the axis 17. For example, one ply 114A may comprise fibers with helical orientation of about ±40°, ±45°, ±50°, ±55°, and/or ±60°, and a second ply 114B may comprise fibers with about an equal but opposite orientation. One or more plies, or one or more fibers within a ply may be substantially axially oriented. Further, the plies 114A, B can include about the same angle of helical orientation. In some embodiments, the different plies 114A, B can have more than one fiber within a ply, such as carbon and glass, and/or carbon and aramid, and/or glass and aramid.
In some embodiments, the abrasion resistant layer 120 may include a polymer. Such abrasion resistant layers can include a tape or coating or other abrasion resistant material, such as a polymer. Polymers may include polyethylene such as, for example, high-density polyethylene and cross-linked polyethylene, polyvinylidene fluoride, polyamide, polypropylene, terphthalates such as polyethylene therphthalate, and polyphenylene sulfide. For example, the abrasion resistant layer may include a polymeric tape that includes one or more polymers such as a polyester, a polyethylene, cross-linked polyethylene, polypropylene, polyethylene terphthalate, high-density polypropylene, polyamide, polyvinylidene fluoride, polyamide, and a elastomer. An exemplary tube as in
The external layer(s) 56 can provide wear resistance and impact resistance. For example, the external layer 56 can provide abrasion resistance and wear resistance by forming an outer surface to the spoolable tube that has a low coefficient of friction thereby reducing the wear on the reinforcing layers from external abrasion. Further, the external layer 56 can provide a seamless layer, to, for example, hold the inner layers 12, 14 of the coiled spoolable tube 10 together. The external layer 56 can be formed of a filled or unfilled polymeric layer. Alternatively, the external layer 56 can be formed of a fiber, such as aramid or glass, with or without a matrix. Accordingly, the external layer 56 can be a polymer, thermoset plastic, a thermoplastic, an elastomer, a rubber, a co-polymer, and/or a composite, where the composite includes a filled polymer and a nano-composite, a polymer/metallic composite, and/or a metal. In some embodiments, the external layer(s) 56 can include one or more of high density polyethylene (HDPE), a cross-linked polyethylene (PEX), a polyvinylidene fluoride (PVDF), a polyamide, polyethylene terphthalate, polyphenylene sulfide and/or a polypropylene. The external layer 56 can include a modulus of elasticity greater than about approximately 50,000 psi, and/or a strength greater than about approximately 1,000 psi. In an embodiment, the external layer 56 can carry at least ten percent, twenty percent, twenty-five percent, thirty percent or even at least fifty percent of an axial load in the longitudinal direction at a termination. A seamless external layer can comprise, for example, a perforated thermoplastic.
In some embodiments, the external layer 56 can be formed by extruding, while the layer 56 can be formed using one or more materials applied at least partially helically and/or at least partially axially along the longitudinal axis 17. The material can include, for example, one or more polymeric tapes. In an example embodiment, the external layer 56 can include and/or otherwise have a coefficient of friction less than a coefficient of friction of a reinforcing layer 14.
Particles can be added to the external layer 56 to increase the wear resistance of the external layer 56. The particles used can include one or more of ceramics, metallics, polymerics, silicas, or fluorinated polymers. For example, adding TEFLON (MP 1300) particles and an aramid powder (PD-T polymer) to the external layer 56 can reduce friction and enhance wear resistance.
It can be understood that pressure from fluids transported by the spoolable tubes 10 disclosed herein may not be properly released from the reinforcing layer(s) 14, and/or from the inner pressure barrier liner and/or from within the external layer, without, for example, an external layer having a permeability to provide such pressure release. Such accumulation of pressure can cause deterioration of the spoolable pipe 10, for example, external layer rupture or inner pressure barrier collapse. Accordingly, in some embodiments, to allow for pressure release along the length of the spoolable pipe 10, the external layer(s) 56 can include and/or have a permeability at least five, or at least ten times greater than the permeability of the internal pressure barrier 12. For example, external layer(s) 56 include perforations or holes spaced along the length of tube. Such perforations can, for example, be spaced apart about every 10 ft, about every 20 ft, about every 30 ft, and even about or greater than about every 40 ft. In one embodiment, the external layer 56 can be perforated to achieve a desired permeability, while additionally and optionally, an external layer 56 can include one or more polymeric tapes, and/or may be discontinuous.
The disclosed spoolable tubes 10 can also include one or more couplings or fittings. For example, such couplings may engage with, be attached to, or in contact with one or more of the internal and external layers of a tube, and may act as a mechanical load transfer device. Couplings may engage one or both of the inner liner, the external wear layer or the reinforcing layer. Couplings or fittings may be comprised, for example, of metal or a polymer, or both. In some embodiments, such couplings may allow tubes to be coupled with other metal components. In addition, or alternatively, such couplings or fittings may provide a pressure seal or venting mechanism within or external to the tube. One or more couplings may each independently be in fluid communication with the inner layer and/or in fluid communication with one or more reinforcing layers and/or plies of fibers or abrasion resistant layers, and/or in fluid communication with an external layer. Such couplings may provide venting, to the atmosphere, of any gasses or fluids that may be present in any of the layers between the external layer and the inner layer, inclusive.
With reference to
The disclosed energy conductors 62 can be oriented in at least a partially helical direction relative to a longitudinal 17 axis of the spoolable tube 10, and/or in an axial direction relative to the longitudinal axis 17 of the spoolable tube 10.
A hydraulic control line embodiment of the energy conductor 62 can be either formed of a metal, composite, and/or a polymeric material.
In one embodiment, several energy conductors 62 can power a machine operably coupled to the coiled spoolable tube 10. For instance, a spoolable tube 10 can include three electrical energy conductors that provide a primary line 62, a secondary line 62, and a tertiary line 62 for electrically powering a machine using a three-phase power system. As provided previously herein, the spoolable tube 10 can also include internal pressure barriers 12 for transmitting fluids along the length of the tube 10.
What has thus been described is for example, a spoolable pipe having a wall that includes an internal pressure barrier formed about a longitudinal axis, and a reinforcing layer(s) enclosing the internal pressure barrier. In one embodiment, the reinforcing layer(s) can include fibers having at least a partial helical orientation relative to the longitudinal axis. In another embodiment, the partial helical orientation can be between about approximately thirty and about approximately seventy degrees relative to the longitudinal axis, and the wall can include at least one external layer enclosing the reinforcing layer(s) and having a permeability at least ten times greater than the permeability of the internal pressure barrier. The reinforcing layer(s) and/or fibers in the reinforcing layers can include a coating. The pipe can also include an energy conductor(s) integrated with and/or located between the internal pressure barrier and/or the reinforcing layer(s).
Unless otherwise stated, use of the word “substantially” can be construed to include a precise relationship, condition, arrangement, orientation, and/or other characteristic, and deviations thereof as understood by one of ordinary skill in the art, to the extent that such deviations do not materially affect the disclosed methods and systems.
Throughout the entirety of the present disclosure, use of the articles “a” or “an” to modify a noun can be understood to be used for convenience and to include one, or more than one of the modified noun, unless otherwise specifically stated.
Elements, components, modules, and/or parts thereof that are described and/or otherwise portrayed through the figures to communicate with, be associated with, and/or be based on, something else, can be understood to so communicate, be associated with, and or be based on in a direct and/or indirect manner, unless otherwise stipulated herein.
Although the methods and systems have been described relative to a specific embodiment thereof, they are not so limited. Obviously many modifications and variations may become apparent in light of the above teachings. Many additional changes in the details, materials, and arrangement of parts, herein described and illustrated, can be made by those skilled in the art. Accordingly, it will be understood that the following claims are not to be limited to the embodiments disclosed herein, can include practices otherwise than specifically described, and are to be interpreted as broadly as allowed under the law.
This application is a continuation of U.S. patent application Ser. No. 12/404,513, filed Mar. 16, 2009, which is a continuation of U.S. patent application Ser. No. 11/010,827, filed Dec. 13, 2004, which claims priority to U.S. provisional Patent Application 60/548,638 filed Feb. 27, 2004, all of which are hereby incorporated by reference in their entirety.
Number | Name | Date | Kind |
---|---|---|---|
87993 | Weston | Mar 1869 | A |
142388 | Goble | Sep 1873 | A |
396176 | Simpson | Jan 1889 | A |
418906 | Bosworth | Jan 1890 | A |
482181 | Kellom | Sep 1892 | A |
646887 | Stowe et al. | Apr 1900 | A |
749633 | Seeley | Jan 1904 | A |
1234812 | Simmmons | Jul 1917 | A |
1793455 | Buchanan | Feb 1931 | A |
1890290 | Hargreaves | Dec 1932 | A |
1930285 | Robinson | Oct 1933 | A |
2464416 | Raybould | Mar 1949 | A |
2467520 | Brubaker | Apr 1949 | A |
2481001 | Burckle | Sep 1949 | A |
2624366 | Pugh | Jan 1953 | A |
2648720 | Alexander | Aug 1953 | A |
2690769 | Brown | Oct 1954 | A |
2725713 | Blanchard | Dec 1955 | A |
2742931 | De Ganahl | Apr 1956 | A |
2750569 | Moon | Jun 1956 | A |
2810424 | Swartswelter et al. | Oct 1957 | A |
2969812 | De Ganahl | Jan 1961 | A |
2973975 | Ramberg et al. | Mar 1961 | A |
2991093 | Guarnaschelli | Jul 1961 | A |
3086369 | Brown | Apr 1963 | A |
3116760 | Matthews | Jan 1964 | A |
3170137 | Brandt | Feb 1965 | A |
3212528 | Haas | Oct 1965 | A |
3277231 | Downey et al. | Oct 1966 | A |
3306637 | Press et al. | Feb 1967 | A |
3334663 | Peterson | Aug 1967 | A |
3354292 | Kahn | Nov 1967 | A |
3379220 | Kiuchi et al. | Apr 1968 | A |
3383223 | Rose | May 1968 | A |
3390704 | Woodell | Jul 1968 | A |
3477474 | Mesler | Nov 1969 | A |
3507412 | Carter | Apr 1970 | A |
3522413 | Chrow | Aug 1970 | A |
3554284 | Nystrom | Jan 1971 | A |
3579402 | Goldsworthy et al. | May 1971 | A |
3589135 | Ede et al. | Jun 1971 | A |
3589752 | Spencer et al. | Jun 1971 | A |
3604461 | Matthews | Sep 1971 | A |
3606396 | Prosdocimo et al. | Sep 1971 | A |
3606402 | Medney | Sep 1971 | A |
3612580 | Jones | Oct 1971 | A |
3654967 | Atwell et al. | Apr 1972 | A |
3677978 | Dowbenko et al. | Jul 1972 | A |
3685860 | Schmidt | Aug 1972 | A |
3692601 | Goldsworthy et al. | Sep 1972 | A |
3696332 | Dickson, Jr. et al. | Oct 1972 | A |
3700519 | Carter | Oct 1972 | A |
3701489 | Goldsworthy et al. | Oct 1972 | A |
3728187 | Martin | Apr 1973 | A |
3730229 | D'Onofrio | May 1973 | A |
3734421 | Karlson et al. | May 1973 | A |
3738637 | Goldsworthy et al. | Jun 1973 | A |
3740285 | Goldsworthy et al. | Jun 1973 | A |
3744016 | Davis | Jul 1973 | A |
3769127 | Goldsworthy et al. | Oct 1973 | A |
3773090 | Ghersa et al. | Nov 1973 | A |
3776805 | Hansen | Dec 1973 | A |
3783060 | Goldsworthy et al. | Jan 1974 | A |
3790438 | Lewis et al. | Feb 1974 | A |
3814138 | Courtot | Jun 1974 | A |
3817288 | Ball | Jun 1974 | A |
3828112 | Johansen et al. | Aug 1974 | A |
3856052 | Feucht | Dec 1974 | A |
3858616 | Thiery et al. | Jan 1975 | A |
3860040 | Sullivan | Jan 1975 | A |
3860742 | Medney | Jan 1975 | A |
3866633 | Taylor | Feb 1975 | A |
3901281 | Morrisey | Aug 1975 | A |
3907335 | Burge et al. | Sep 1975 | A |
3913624 | Ball | Oct 1975 | A |
3932559 | Cantor et al. | Jan 1976 | A |
3933180 | Carter | Jan 1976 | A |
3956051 | Carter | May 1976 | A |
3957410 | Goldsworthy et al. | May 1976 | A |
3960629 | Goldsworthy | Jun 1976 | A |
3974862 | Fuhrmann et al. | Aug 1976 | A |
3980325 | Robertson | Sep 1976 | A |
RE29112 | Carter | Jan 1977 | E |
4001442 | Stahlberger et al. | Jan 1977 | A |
4007070 | Busdiecker | Feb 1977 | A |
4013101 | Logan et al. | Mar 1977 | A |
4032177 | Anderson | Jun 1977 | A |
4048807 | Ellers et al. | Sep 1977 | A |
4053343 | Carter | Oct 1977 | A |
4057610 | Goettler et al. | Nov 1977 | A |
4067916 | Jaeger et al. | Jan 1978 | A |
4095865 | Denison et al. | Jun 1978 | A |
4104095 | Shaw | Aug 1978 | A |
4108701 | Stanley | Aug 1978 | A |
4111237 | Mutzner et al. | Sep 1978 | A |
4111469 | Kavick | Sep 1978 | A |
4114393 | Engle, Jr. et al. | Sep 1978 | A |
4119122 | de Putter | Oct 1978 | A |
4125423 | Goldsworthy | Nov 1978 | A |
4133972 | Andersson et al. | Jan 1979 | A |
4137949 | Linko, III et al. | Feb 1979 | A |
4139025 | Carlstrom et al. | Feb 1979 | A |
4148963 | Bourrain et al. | Apr 1979 | A |
4190088 | Lalikos et al. | Feb 1980 | A |
4200126 | Fish | Apr 1980 | A |
4220381 | van der Graaf et al. | Sep 1980 | A |
4226446 | Burrington | Oct 1980 | A |
4241763 | Antal et al. | Dec 1980 | A |
4248062 | McLain et al. | Feb 1981 | A |
4261390 | Belofsky | Apr 1981 | A |
4273160 | Lowles | Jun 1981 | A |
4303263 | Legris | Dec 1981 | A |
4303457 | Johansen et al. | Dec 1981 | A |
4306591 | Arterburn | Dec 1981 | A |
4307756 | Voigt et al. | Dec 1981 | A |
4308999 | Carter | Jan 1982 | A |
4330017 | Satoh et al. | May 1982 | A |
4336415 | Walling | Jun 1982 | A |
4351364 | Cocks et al. | Sep 1982 | A |
4380252 | Gray et al. | Apr 1983 | A |
4385644 | Kaempen | May 1983 | A |
4402346 | Cheetham et al. | Sep 1983 | A |
4421806 | Marks et al. | Dec 1983 | A |
4422801 | Hale et al. | Dec 1983 | A |
4434816 | Di Giovanni et al. | Mar 1984 | A |
4445734 | Cunningham | May 1984 | A |
4446892 | Maxwell et al. | May 1984 | A |
4447378 | Gray et al. | May 1984 | A |
4463779 | Wink et al. | Aug 1984 | A |
4469729 | Watanabe et al. | Sep 1984 | A |
4488577 | Shilad et al. | Dec 1984 | A |
4507019 | Thompson | Mar 1985 | A |
4515737 | Karino et al. | May 1985 | A |
4522058 | Ewing | Jun 1985 | A |
4522235 | Kluss et al. | Jun 1985 | A |
4530379 | Policelli | Jul 1985 | A |
4556340 | Morton | Dec 1985 | A |
4567916 | Antal et al. | Feb 1986 | A |
4578675 | MacLeod | Mar 1986 | A |
4606378 | Meyer et al. | Aug 1986 | A |
4627472 | Goettler et al. | Dec 1986 | A |
4652475 | Haney et al. | Mar 1987 | A |
4657795 | Foret et al. | Apr 1987 | A |
4681169 | Brookbank, III | Jul 1987 | A |
4700751 | Fedrick | Oct 1987 | A |
4712813 | Passerell et al. | Dec 1987 | A |
4728224 | Salama et al. | Mar 1988 | A |
4741795 | Grace et al. | May 1988 | A |
4758455 | Campbell et al. | Jul 1988 | A |
4789007 | Cretel et al. | Dec 1988 | A |
4842024 | Palinchak | Jun 1989 | A |
4844516 | Baker | Jul 1989 | A |
4849668 | Crawley et al. | Jul 1989 | A |
4854349 | Foreman | Aug 1989 | A |
4859024 | Rahman | Aug 1989 | A |
4869293 | Botsolas | Sep 1989 | A |
4903735 | Delacour et al. | Feb 1990 | A |
4913657 | Naito et al. | Apr 1990 | A |
4936618 | Sampa et al. | Jun 1990 | A |
4941774 | Harmstorf et al. | Jul 1990 | A |
4942903 | Jacobsen et al. | Jul 1990 | A |
4972880 | Strand | Nov 1990 | A |
4992787 | Helm | Feb 1991 | A |
4995761 | Barton | Feb 1991 | A |
5024252 | Ochsner | Jun 1991 | A |
5048572 | Levine | Sep 1991 | A |
5077107 | Kaneda et al. | Dec 1991 | A |
5090741 | Yokomatsu et al. | Feb 1992 | A |
5097870 | Williams | Mar 1992 | A |
5156206 | Cox | Oct 1992 | A |
5170011 | Martucci | Dec 1992 | A |
5172765 | Sas-Jaworsky et al. | Dec 1992 | A |
5176180 | Williams et al. | Jan 1993 | A |
5182779 | D'Agostino et al. | Jan 1993 | A |
5184682 | Delacour et al. | Feb 1993 | A |
5188872 | Quigley | Feb 1993 | A |
5209136 | Williams | May 1993 | A |
5222769 | Kaempen | Jun 1993 | A |
5261462 | Wolfe et al. | Nov 1993 | A |
5265648 | Lyon | Nov 1993 | A |
5285008 | Sas-Jaworsky et al. | Feb 1994 | A |
5285204 | Sas-Jaworsky | Feb 1994 | A |
5330807 | Williams | Jul 1994 | A |
5332269 | Homm | Jul 1994 | A |
5334801 | Mohn et al. | Aug 1994 | A |
5346658 | Gargiulo | Sep 1994 | A |
5348088 | Laflin et al. | Sep 1994 | A |
5348096 | Williams | Sep 1994 | A |
5351752 | Wood et al. | Oct 1994 | A |
RE34780 | Trenconsky et al. | Nov 1994 | E |
5364130 | Thalmann | Nov 1994 | A |
5373870 | Derroire et al. | Dec 1994 | A |
5394488 | Fernald et al. | Feb 1995 | A |
5395913 | Bottcher et al. | Mar 1995 | A |
5398729 | Spurgat | Mar 1995 | A |
5416724 | Savic | May 1995 | A |
5426297 | Dunphy et al. | Jun 1995 | A |
5428706 | Lequeux et al. | Jun 1995 | A |
5435867 | Wolfe et al. | Jul 1995 | A |
5437311 | Reynolds | Aug 1995 | A |
5437899 | Quigley | Aug 1995 | A |
5443099 | Chaussepied et al. | Aug 1995 | A |
5452923 | Smith | Sep 1995 | A |
5460416 | Freidrich et al. | Oct 1995 | A |
RE35081 | Quigley | Nov 1995 | E |
5469916 | Sas-Jaworsky et al. | Nov 1995 | A |
5472764 | Kehr et al. | Dec 1995 | A |
5494374 | Youngs et al. | Feb 1996 | A |
5499661 | Odru et al. | Mar 1996 | A |
5507320 | Plumley | Apr 1996 | A |
5524937 | Sides, III et al. | Jun 1996 | A |
5525698 | Bottcher et al. | Jun 1996 | A |
5538513 | Okajima et al. | Jul 1996 | A |
5551484 | Charboneau | Sep 1996 | A |
5558375 | Newman | Sep 1996 | A |
5622211 | Martin et al. | Apr 1997 | A |
5641956 | Vengsarkar et al. | Jun 1997 | A |
5671811 | Head et al. | Sep 1997 | A |
5679425 | Plumley | Oct 1997 | A |
5683204 | Lawther et al. | Nov 1997 | A |
5692545 | Rodrigue | Dec 1997 | A |
5718956 | Gladfelter et al. | Feb 1998 | A |
5730188 | Kalman et al. | Mar 1998 | A |
5755266 | Aanonsen et al. | May 1998 | A |
5758990 | Davies et al. | Jun 1998 | A |
5785091 | Barker, II | Jul 1998 | A |
5795102 | Corbishley et al. | Aug 1998 | A |
5797702 | Drost et al. | Aug 1998 | A |
5798155 | Yanagawa et al. | Aug 1998 | A |
5804268 | Mukawa et al. | Sep 1998 | A |
5826623 | Akiyoshi et al. | Oct 1998 | A |
5828003 | Thomeer et al. | Oct 1998 | A |
5865216 | Youngs | Feb 1999 | A |
5868169 | Catallo | Feb 1999 | A |
5875792 | Campbell, Jr. et al. | Mar 1999 | A |
5908049 | Williams et al. | Jun 1999 | A |
5913337 | Williams et al. | Jun 1999 | A |
5913357 | Hanazaki et al. | Jun 1999 | A |
5921285 | Quigley et al. | Jul 1999 | A |
5933945 | Thomeer et al. | Aug 1999 | A |
5950651 | Kenworthy et al. | Sep 1999 | A |
5951812 | Gilchrist, Jr. | Sep 1999 | A |
5979506 | Aarseth | Nov 1999 | A |
5984581 | McGill et al. | Nov 1999 | A |
5988702 | Sas-Jaworsky | Nov 1999 | A |
6004639 | Quigley et al. | Dec 1999 | A |
6016845 | Quigley et al. | Jan 2000 | A |
6032699 | Cochran et al. | Mar 2000 | A |
6065540 | Thomeer et al. | May 2000 | A |
6066377 | Tonyali et al. | May 2000 | A |
6076561 | Akedo et al. | Jun 2000 | A |
6093752 | Park et al. | Jul 2000 | A |
6109306 | Kleinert | Aug 2000 | A |
6136216 | Fidler et al. | Oct 2000 | A |
6148866 | Quigley et al. | Nov 2000 | A |
6209587 | Hsich et al. | Apr 2001 | B1 |
6220079 | Taylor et al. | Apr 2001 | B1 |
6286558 | Quigley et al. | Sep 2001 | B1 |
6315002 | Antal et al. | Nov 2001 | B1 |
6328075 | Furuta et al. | Dec 2001 | B1 |
6334466 | Jani et al. | Jan 2002 | B1 |
6357485 | Quigley et al. | Mar 2002 | B2 |
6357966 | Thompson et al. | Mar 2002 | B1 |
6361299 | Quigley et al. | Mar 2002 | B1 |
6372861 | Schillgalies et al. | Apr 2002 | B1 |
6390140 | Niki et al. | May 2002 | B2 |
6402430 | Guesnon et al. | Jun 2002 | B1 |
6422269 | Johansson et al. | Jul 2002 | B1 |
6461079 | Beaujean et al. | Oct 2002 | B1 |
6470915 | Enders et al. | Oct 2002 | B1 |
6532994 | Enders et al. | Mar 2003 | B1 |
6557485 | Sauter et al. | May 2003 | B1 |
6604550 | Quigley et al. | Aug 2003 | B2 |
6620475 | Reynolds, Jr. et al. | Sep 2003 | B1 |
6631743 | Enders et al. | Oct 2003 | B2 |
6634387 | Glejbøl et al. | Oct 2003 | B1 |
6634388 | Taylor et al. | Oct 2003 | B1 |
6634675 | Parkes | Oct 2003 | B2 |
6663453 | Quigley et al. | Dec 2003 | B2 |
6706348 | Quigley et al. | Mar 2004 | B2 |
6706398 | Revis | Mar 2004 | B1 |
6746737 | Debalme et al. | Jun 2004 | B2 |
6764365 | Quigley et al. | Jul 2004 | B2 |
6773774 | Crook et al. | Aug 2004 | B1 |
6787207 | Lindstrom et al. | Sep 2004 | B2 |
6803082 | Nichols et al. | Oct 2004 | B2 |
6807988 | Powell et al. | Oct 2004 | B2 |
6807989 | Enders et al. | Oct 2004 | B2 |
6857452 | Quigley et al. | Feb 2005 | B2 |
6889716 | Lundberg et al. | May 2005 | B2 |
6902205 | Bouey et al. | Jun 2005 | B2 |
6978804 | Quigley et al. | Dec 2005 | B2 |
6983766 | Baron et al. | Jan 2006 | B2 |
7021339 | Hagiwara et al. | Apr 2006 | B2 |
7029356 | Quigley et al. | Apr 2006 | B2 |
7080667 | McIntyre et al. | Jul 2006 | B2 |
7152632 | Quigley et al. | Dec 2006 | B2 |
7234410 | Quigley et al. | Jun 2007 | B2 |
7243716 | Denniel et al. | Jul 2007 | B2 |
7285333 | Wideman et al. | Oct 2007 | B2 |
7328725 | Henry et al. | Feb 2008 | B2 |
7498509 | Brotzell et al. | Mar 2009 | B2 |
7523765 | Quigley et al. | Apr 2009 | B2 |
7600537 | Bhatnagar et al. | Oct 2009 | B2 |
8187687 | Wideman et al. | May 2012 | B2 |
20010006712 | Hibino et al. | Jul 2001 | A1 |
20010013669 | Cundiff et al. | Aug 2001 | A1 |
20010025664 | Quigley et al. | Oct 2001 | A1 |
20020081083 | Griffioen et al. | Jun 2002 | A1 |
20020094400 | Lindstrom et al. | Jul 2002 | A1 |
20020119271 | Quigley et al. | Aug 2002 | A1 |
20020185188 | Quigley et al. | Dec 2002 | A1 |
20030008577 | Quigley et al. | Jan 2003 | A1 |
20030087052 | Wideman et al. | May 2003 | A1 |
20040014440 | Makela et al. | Jan 2004 | A1 |
20040025951 | Baron et al. | Feb 2004 | A1 |
20040052997 | Santo | Mar 2004 | A1 |
20040074551 | McIntyre | Apr 2004 | A1 |
20040096614 | Quigley et al. | May 2004 | A1 |
20040265524 | Wideman et al. | Dec 2004 | A1 |
20050087336 | Surjaatmadja et al. | Apr 2005 | A1 |
20050189029 | Quigley et al. | Sep 2005 | A1 |
20070125439 | Quigley et al. | Jun 2007 | A1 |
20070154269 | Quigley et al. | Jul 2007 | A1 |
20070246459 | Loveless et al. | Oct 2007 | A1 |
20080006337 | Quigley et al. | Jan 2008 | A1 |
20080006338 | Wideman et al. | Jan 2008 | A1 |
20080014812 | Quigley et al. | Jan 2008 | A1 |
20080185042 | Feechan et al. | Aug 2008 | A1 |
20080210329 | Quigley et al. | Sep 2008 | A1 |
20090090460 | Wideman et al. | Apr 2009 | A1 |
20090107558 | Quigley et al. | Apr 2009 | A1 |
20090173406 | Quigley et al. | Jul 2009 | A1 |
20090278348 | Brotzell et al. | Nov 2009 | A1 |
20100101676 | Quigley et al. | Apr 2010 | A1 |
Number | Date | Country |
---|---|---|
559688 | Aug 1957 | BE |
461199 | Aug 1968 | CH |
1959738 | Aug 1987 | DE |
3603597 | Aug 1987 | DE |
4040400 | Aug 1992 | DE |
4214383 | Sep 1993 | DE |
199505448 | Aug 2000 | DE |
0024512 | Mar 1981 | EP |
0024512 | Mar 1981 | EP |
0024512 | Mar 1981 | EP |
0203887 | Dec 1986 | EP |
0352148 | Jan 1990 | EP |
0427306 | May 1991 | EP |
0477704 | Apr 1992 | EP |
0503737 | Sep 1992 | EP |
505815 | Sep 1992 | EP |
505815 | Sep 1992 | EP |
0536844 | Apr 1993 | EP |
0681085 | Nov 1995 | EP |
0854029 | Jul 1998 | EP |
0854029 | Jul 1998 | EP |
0953724 | Nov 1999 | EP |
0970980 | Jan 2000 | EP |
0981992 | Mar 2000 | EP |
989204 | Sep 1951 | FR |
553110 | May 1943 | GB |
809097 | Feb 1959 | GB |
909187 | Oct 1962 | GB |
956500 | Apr 1964 | GB |
1297250 | Nov 1972 | GB |
2103744 | Feb 1983 | GB |
2159901 | Dec 1985 | GB |
2 193 006 | Jan 1988 | GB |
2255994 | Nov 1992 | GB |
2270099 | Mar 1994 | GB |
2365096 | Feb 2002 | GB |
163 592 | Jun 1990 | JP |
WO-8704768 | Aug 1987 | WO |
WO-9113925 | Sep 1991 | WO |
WO-9221908 | Dec 1992 | WO |
WO-9307073 | Apr 1993 | WO |
WO-9319927 | Oct 1993 | WO |
WO-9502782 | Jan 1995 | WO |
WO-9712115 | Apr 1997 | WO |
WO-9712166 | Apr 1997 | WO |
WO-9919653 | Apr 1999 | WO |
WO-0031458 | Jun 2000 | WO |
WO-0073695 | Dec 2000 | WO |
WO-2006003208 | Jan 2006 | WO |
Entry |
---|
Austigard et al. “Composites Subsea: Cost Effective Prodcuts; an Industry Challenge” Subsea 94 International Conference, the 1994 Report on Subsea Engineering: The Continuing Challenges. |
Connell et al. “Coiled Tubing: Application for Today's Challenges” Petroleum Engineer International, pp. 18-21 (Jul. 1999). |
Dalmolen “The Properties, Qualification, and System Design of, and Field Experiences with Reinforced Thermoplastic Pipe for Oil and Gas Applications” NACE International, 2003 West Conference (Feb. 2003). |
Feechan et al. “Spoolable Composites Show Promise” The American Oil & Gas Reporter, pp. 44-50 (Sep. 1999). |
Fiberspar Tech Notes, “Horizontal well deliquification just got easier-with Fiberspar Spoolable Production Systems,” TN21-R1UN1-HybridLift, 2010, 2 pages. |
Fowler “Advanced Composite Tubing Usable” The American Oil & Gas Reporter, pp. 76-81 (Sep. 1997). |
Fowler et al. “Development Update and Applicaitons of an Advanced Composite Spoolable Tubing” Offshore Technology Conference held in Houston, Texas from May 4-7, 1988, pp. 157-162. |
Hahn et al. “Compression Failure Mechanism s in Unidirecitonal Composites” NASA Technical Memorandum pp. 1-42 (Aug. 1984). |
Hansen et al. “Qualification and Verificaiton of Spoolable High Pressure Composite Services Lines for the Asgard Field Development Project” paper presented at the 1997 Offshore Technology Conference held in Houston, Texas from May 5-8, 1997, pp. 45-54. |
Hartman et al. “High Strength Glass Fibers” Owens Corning Technical Paper (Jul. 1996). |
Haug et al. “Dynamic Umbilical with Composite Tube (DUCT)” Paper presented at the 1998 Offshore Tehnology Conference held in Houston, Texas from May 4-7, 1998; pp. 699-712. |
International Search Report for PCT/US2000/26977 mailed on Jan. 22, 2001, (3 pages). |
International Search Report for PCT/US2000/41073 mailed on Mar. 5, 2001, (3 pages). |
International Search Report for PCT/US2004/16093 mailed on Nov. 8, 2005, (9 pages). |
International Search Report and Written Opinion for PCT/US2010/060582 mailed on Feb. 16, 2011, (11 pages). |
Lundberg et al.; “Spin-off Technologies from Development of Continuous Composite Tubing Manufacturing Process”, Paper presented at the 1998 Offshore Technology Conference held in Houston, Texas from May 4-7, 1998 pp. 149-155. |
Marker et al.; “Anaconda: Joint Development Project Leads to Digitally Controlled Composite Coiled Tubing Drilling System”, Paper presented at the SPEI/COTA, Coiled Tubing Roundtable held in Houston, Texas from Apr. 5-6, 2000, pp. 1-9. |
Measures et al.; “Fiber Optic Sensors for Smart Structures,” Optics and Lasers Engineering 16: 127-152 (1992). |
Measures R. M.; “Smart Structures with Nerves of Glass”. Prog. Aerospace Sci. 26(4): 289-351 (1989). |
Mesch, K.A., “Heat Stabilizers,” Kirk-Othmer Encyclopedia of Chemical Technology, 2000 pp. 1-20. |
Moe Wood T. et al.; “Spoolable, Composite Piping for Chemical and Water Injection and Hydraulic Valve Operation”, Proceedings of the 11th International Conference on Offshore Mechanics and Arctic Engineering-I 992-, vol. III, Part A—Materials Engineering, pp. 199-207 (1992). |
Proper Peter; “Braiding”, International Encyclopedia of Composites, Published by VGH, Publishers, Inc., 220 East 23rd Street, Suite 909, New York, NY I0010. |
Quigley et al. “Development and Application of a Novel Coiled Tubing String for Concentric Workover Services ”Paper presented at the 1997 Offshore Technology Conference held in Houston, Texas from May 5-8, 1997, pp. 189-202. |
Rispler et al. “Composite Coiled Tubing in Harsh Completion/Workover Environments” Paper presented at the SPE GAS Technology Symposium and Exhibition held in Calgary, Alberta, Canada on Mar. 15-18, 1998, pp. 405-410. |
Sas-Jaworsky et al. “Advanced composites enhance coiled tubing capabilities” World Oil, pp. 57-69 (Apr. 1994). |
Sas-Jaworsky et al. “Coiled Tubing 1995 Update: Prodcution Applications ” World Oil, 216(6): 97 (Jun. 1995). |
Sas-Jaworsky et al. “Development of a composite coiled tubing for oilfield services” Society of Petroleum Engineers, SPE 26536, pp. 1-11 (1993). |
Sas-Jaworsky et al. “Developments Position CT for Future Prominense” The Amreican Oil & Gas Reporter, pp. 87-92 (Mar. 1996). |
Sas-Jaworsky et al. “Enabling capabilities and potential applications of composite coiled tubing ”Proceedings of World Oil's 2nd International Conference on Coiled Tubing Technology, pp. 2-9 (1994). |
Sas-Jaworsky et al. “Innovative Applications Stimulate Coiled Tubing Devleopment” World Oil, 217(6): 61 (Jun. 1996). |
Shuart et al. “Compression Behavior of ≠45° Dominated Laminates with a Circular Hole or Impact Damage” AIAA Journal 24(1): pp. 115-122 (Jan. 1986). |
Silverman “Spoolable Composite Pipe for Offshore Applications” Materials Selection & Design, pp. 48-50 (Jan. 1997). |
Sperling, L.H., “Introduction to Physical Polymer Science 3rd Edition,” Wiley-Interscience, New York, NY, 2001, p. 100. |
Tore Wood Moe et al. “Spoolable, Composite Piping for Chemical and Water Injection and Hydraulic Valve Operation” Proceedings of the 11th International Conference on Offshore Mechanics and Arctic Engineering 1992, vol. III, Part A—Materials Engineering, pp. 199-207 (1992). |
Williams et al. “Composite Spoolable Pipe Development, Advancements, and Limitations” Paper presneted at the 2000 Offshore Technology Conference held in Houston, Texas from May 1-4, 2000, pp. 1-16. |
Williams, J.G., “Oil Industry Experiences with Fiberglass Components,” Offfshore Technology Conference, Houston, Texas, Apr. 27-30, 1987, pp. 211-220. |
Number | Date | Country | |
---|---|---|---|
20120118423 A1 | May 2012 | US |
Number | Date | Country | |
---|---|---|---|
60548638 | Feb 2004 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 12404513 | Mar 2009 | US |
Child | 13183292 | US | |
Parent | 11010827 | Dec 2004 | US |
Child | 12404513 | US |