US20060191311A1 - Flexible pipe and method of manufacturing same - Google Patents
Flexible pipe and method of manufacturing same Download PDFInfo
- Publication number
- US20060191311A1 US20060191311A1 US11/400,617 US40061706A US2006191311A1 US 20060191311 A1 US20060191311 A1 US 20060191311A1 US 40061706 A US40061706 A US 40061706A US 2006191311 A1 US2006191311 A1 US 2006191311A1
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- US
- United States
- Prior art keywords
- wires
- tensile layer
- layer
- wrapping
- tubular member
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D23/00—Producing tubular articles
- B29D23/001—Pipes; Pipe joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C37/00—Manufacture of metal sheets, rods, wire, tubes, profiles or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
- B21C37/06—Manufacture of metal sheets, rods, wire, tubes, profiles or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
- B21C37/15—Making tubes of special shape; Making tube fittings
- B21C37/154—Making multi-wall tubes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L11/00—Hoses, i.e. flexible pipes
- F16L11/04—Hoses, i.e. flexible pipes made of rubber or flexible plastics
- F16L11/08—Hoses, i.e. flexible pipes made of rubber or flexible plastics with reinforcements embedded in the wall
- F16L11/081—Hoses, i.e. flexible pipes made of rubber or flexible plastics with reinforcements embedded in the wall comprising one or more layers of a helically wound cord or wire
- F16L11/082—Hoses, i.e. flexible pipes made of rubber or flexible plastics with reinforcements embedded in the wall comprising one or more layers of a helically wound cord or wire two layers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L11/00—Hoses, i.e. flexible pipes
- F16L11/04—Hoses, i.e. flexible pipes made of rubber or flexible plastics
- F16L11/08—Hoses, i.e. flexible pipes made of rubber or flexible plastics with reinforcements embedded in the wall
- F16L11/081—Hoses, i.e. flexible pipes made of rubber or flexible plastics with reinforcements embedded in the wall comprising one or more layers of a helically wound cord or wire
- F16L11/083—Hoses, i.e. flexible pipes made of rubber or flexible plastics with reinforcements embedded in the wall comprising one or more layers of a helically wound cord or wire three or more layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2023/00—Tubular articles
- B29L2023/005—Hoses, i.e. flexible
Definitions
- the present invention relates to a relative low-cost flexible pipe formed by multiple layers of different materials and suitable for use in subsea and land-based applications.
- FIG. 1 is a longitudinal sectional view of a flexible pipe according to an embodiment of the present invention.
- FIG. 2 is a longitudinal sectional view of a flexible pipe according to another embodiment of the present invention.
- FIGS. 3A-3C are longitudinal sectional views of alternative embodiments of a layer of the pipes of the embodiments of FIGS. 1 and 2 .
- a flexible pipe according to an embodiment of the present invention is shown, in general by the reference numeral 10 .
- the pipe 10 is formed by an inner tubular member, preferably in the form of a plastic sheath 12 for conveying fluid through its bore.
- the sheath may be formed in a conventional manner using polymers, or the like.
- a layer 14 is wrapped around the sheath 12 and provides resistance to internal pressure, hydrostatic collapse and crush.
- the layer 14 is formed by helically wrapping a continuous metal strip, preferably formed of carbon steel, with adjacent windings being interlocked, to form a flexible layer that provides significant hoop and axial strength.
- the layer 14 is marketed by the assignee of the present invention, Wellstream, Inc., under the “Flexlok” trademark.
- a wrapped wire assembly 16 extends over the layer 14 and consists of a series of wires 16 a helically wrapped around the exterior of the layer 14 to form a first tensile layer, and an additional series of wires 16 b wrapped around the first series of wires 16 a to form a second tensile layer extending over the first tensile layer.
- the wires 16 a and 16 b have a substantially circular cross section, and are wound at a relatively high lay angle to provide significant hoop strength and axial strength.
- at least a portion of the wires 16 a and 16 b are formed by carbon steel with an anodic coating. It is noted that the layer 14 prevents the expansion of the sheath 12 into gaps formed between the wires of the tensile layers 16 a and 16 b.
- the tape 18 can be formed by plastic or metal and can be reinforced with glass, metal or a stronger plastic. Although not shown in the drawings, it is understood that the tape 18 can also extend between the layer 14 and the wire assembly 16 , and between the series of wires 16 a and 16 b.
- a protective outer insulative sheath 20 extends over the tape 18 and is preferably extruded over the tape 18 in a conventional manner, with the tape providing a smooth surface for the extrusion.
- the sheath 20 is optional and is required only when the tape 18 is inadequate to protect the remaining components of the pipe 10 .
- FIG. 2 depicts a pipe 10 ′ that is similar to the pipe 10 of FIG. 1 and includes some components of FIG. 1 which are given the same reference numerals.
- a wrapped wire assembly 26 extends over the layer 14 and consists of a series of wires 26 a and 26 b which are substantially rectangular in cross section.
- the wires 26 a are helically wrapped around the exterior of the layer 14 to form a first tensile layer, and the wires 26 b wrapped around the first series of wires 26 a to form a second tensile layer extending over the first tensile layer.
- the rectangular profile of the wires 26 a and 26 b is achieved by unwinding the coiled wires from a mandrel, or the like, and passing the wires through opposed rollers which flatten the wires to a substantially rectangular cross section.
- an elongated sheet is payed out from a coil and a plurality of spaced cutters are placed in the path of the sheet to slit the sheet in to a plurality of wires.
- the cutters are spaced in a manner to form a plurality of wires having a rectangular cross section.
- wrapped tape identical to the tape layer 18 , can also extend between the layer 14 and the wire assembly 26 , and between the series of wires 26 a and 26 b.
- an inner layer 28 is provided inside the sheath 12 .
- the layer 28 is preferably formed by a plurality of helically wrapped, corrugated and/or interlocked strips to provide additional collapse and radial compression resistance. If the layer 28 is added, the sheath 12 would be extruded over the outer surface of the layer 24 .
- both the wire assembly 26 and the layer 28 can be included in the pipe 10 and/or 10 ′, or one can be included without the other.
- FIGS. 3A-3C are alternative embodiments of the layer 14 which can be used with the pipe 10 and/or the pipe 10 ′.
- a continuous metal strip 30 preferably of carbon steel, is helically wrapped around the adjacent inner member (not shown).
- Two adjacent inner windings are shown by the reference numerals 30 a and 30 b
- three adjacent outer windings are shown by the reference numerals 30 c , 30 d , and 30 e , respectively.
- the wrapping of the strip 30 is such that the winding 30 d overlaps the windings 30 a and 30 b , the winding 30 c overlaps the winding 30 a and its adjacent inner winding (not shown), and the winding 30 e overlaps the winding 30 b and its adjacent inner winding (not shown), and so on.
- the strip 30 is wound in this manner for length of the pipes 10 or 10 ′, and it is understood that the number of radially spaced windings, and therefore the thickness of the layer thus formed can vary.
- a continuous metal strip 34 preferably of carbon steel, is helically wrapped around the adjacent inner member (not shown).
- the strip 34 is shaped, or formed, in any known manner to form a cross section having a first substantially horizontal inner portion 34 a , and second substantially horizontal portion 34 b that is spaced radially outwardly from the inner portion 34 a , and a bent portion 34 c extending between the portions 34 a and 34 b .
- the strip 34 is preferably of carbon steel and is helically wrapped around the adjacent inner member (not shown).
- the wrapping of the strip 34 is such that the portion 34 b overlaps the inner portion of its adjacent winding, and the portion 34 a is overlapped by the outer portion of its adjacent winding, to thus achieve an interlocking effect.
- the strip 34 is wrapped for the length of the pipes 10 or 10 ′, and it is understood that the number of radially spaced windings, and therefore the thickness of the layer thus formed can vary.
- a continuous metal strip 38 preferably of carobon steel, is helically wrapped around the adjacent inner member (now shown).
- the strip 38 is shaped, or formed, in any known manner to form a cross section having a convex portion 38 a extending from a concave portion 38 b .
- the wrapping of the strip 38 is such that the convex portion 38 a overlaps the concave portion of its adjacent winding and the concave portion 38 a is overlapped by the convex portion of its adjacent winding to thus achieve an interlocking effect.
- the strip 38 is wrapped for the length of the pipes 10 or 10 , and it is understood that the number of radially spaced windings, and therefore the thickness of the layer thus formed can vary.
- additional tensile layers of wires can be provided in addition to the series of wires 16 a and 16 b in the pipe 10 and the series of wires 26 a and 26 b in pipe 10 ′.
- the carbon steel strip layer 14 can be omitted from each of the above embodiments in which case the first tensile layer 16 a would be wound directly onto the sheath 12 .
- an optional wrapped tape similar to the tape 18 could be provided that extends between the sheath 12 and the first tensile layer 16 a.
- an outer layer similar to the layer 14 can be placed around the sheath 20 for added protection, in each of the embodiments.
- an outer layer similar to the layer 14 can be placed around the sheath 20 for added protection.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
- Laminated Bodies (AREA)
Abstract
Description
- This application is a continuation application of U.S. Ser. No. 09/706,070, filed Nov. 3, 2000, which claims priority of provisional application Ser. No. 60/163,908 filed Nov. 5, 1999.
- The present invention relates to a relative low-cost flexible pipe formed by multiple layers of different materials and suitable for use in subsea and land-based applications.
-
FIG. 1 is a longitudinal sectional view of a flexible pipe according to an embodiment of the present invention. -
FIG. 2 is a longitudinal sectional view of a flexible pipe according to another embodiment of the present invention. -
FIGS. 3A-3C are longitudinal sectional views of alternative embodiments of a layer of the pipes of the embodiments ofFIGS. 1 and 2 . - With reference to
FIG. 1 , a flexible pipe according to an embodiment of the present invention is shown, in general by thereference numeral 10. Thepipe 10 is formed by an inner tubular member, preferably in the form of aplastic sheath 12 for conveying fluid through its bore. The sheath may be formed in a conventional manner using polymers, or the like. - A
layer 14 is wrapped around thesheath 12 and provides resistance to internal pressure, hydrostatic collapse and crush. Thelayer 14 is formed by helically wrapping a continuous metal strip, preferably formed of carbon steel, with adjacent windings being interlocked, to form a flexible layer that provides significant hoop and axial strength. Thelayer 14 is marketed by the assignee of the present invention, Wellstream, Inc., under the “Flexlok” trademark. - A wrapped
wire assembly 16 extends over thelayer 14 and consists of a series of wires 16 a helically wrapped around the exterior of thelayer 14 to form a first tensile layer, and an additional series ofwires 16 b wrapped around the first series of wires 16 a to form a second tensile layer extending over the first tensile layer. Thewires 16 a and 16 b have a substantially circular cross section, and are wound at a relatively high lay angle to provide significant hoop strength and axial strength. Preferably, at least a portion of thewires 16 a and 16 b are formed by carbon steel with an anodic coating. It is noted that thelayer 14 prevents the expansion of thesheath 12 into gaps formed between the wires of thetensile layers 16 a and 16 b. - One or more layers of a
tape 18 are helically wrapped over thewire assembly 16. Thetape 18 can be formed by plastic or metal and can be reinforced with glass, metal or a stronger plastic. Although not shown in the drawings, it is understood that thetape 18 can also extend between thelayer 14 and thewire assembly 16, and between the series ofwires 16 a and 16 b. - A protective outer
insulative sheath 20 extends over thetape 18 and is preferably extruded over thetape 18 in a conventional manner, with the tape providing a smooth surface for the extrusion. Thesheath 20 is optional and is required only when thetape 18 is inadequate to protect the remaining components of thepipe 10. -
FIG. 2 depicts apipe 10′ that is similar to thepipe 10 ofFIG. 1 and includes some components ofFIG. 1 which are given the same reference numerals. In the embodiment ofFIG. 2 , a wrappedwire assembly 26 extends over thelayer 14 and consists of a series ofwires 26 a and 26 b which are substantially rectangular in cross section. The wires 26 a are helically wrapped around the exterior of thelayer 14 to form a first tensile layer, and thewires 26 b wrapped around the first series of wires 26 a to form a second tensile layer extending over the first tensile layer. - According to an embodiment of the method of the invention, the rectangular profile of the
wires 26 a and 26 b is achieved by unwinding the coiled wires from a mandrel, or the like, and passing the wires through opposed rollers which flatten the wires to a substantially rectangular cross section. - According to an alternate method of forming the
wires 26 a and 26 b an elongated sheet is payed out from a coil and a plurality of spaced cutters are placed in the path of the sheet to slit the sheet in to a plurality of wires. The cutters are spaced in a manner to form a plurality of wires having a rectangular cross section. - Both of the above methods avoid the high expense of specialized rolling mills in which coils of round carbon steel wire are processed through repeated roll forming and heat treating operations.
- Also, in the embodiment of
FIG. 2 it is understood that wrapped tape, identical to thetape layer 18, can also extend between thelayer 14 and thewire assembly 26, and between the series ofwires 26 a and 26 b. - Also according to the embodiment of
FIG. 2 , aninner layer 28 is provided inside thesheath 12. Thelayer 28 is preferably formed by a plurality of helically wrapped, corrugated and/or interlocked strips to provide additional collapse and radial compression resistance. If thelayer 28 is added, thesheath 12 would be extruded over the outer surface of the layer 24. - It is emphasized that both the
wire assembly 26 and thelayer 28 can be included in thepipe 10 and/or 10′, or one can be included without the other. -
FIGS. 3A-3C are alternative embodiments of thelayer 14 which can be used with thepipe 10 and/or thepipe 10′. Referring toFIG. 3A , acontinuous metal strip 30, preferably of carbon steel, is helically wrapped around the adjacent inner member (not shown). Two adjacent inner windings are shown by thereference numerals 30 a and 30 b, and three adjacent outer windings are shown by the 30 c, 30 d, and 30 e, respectively. The wrapping of thereference numerals strip 30 is such that the winding 30 d overlaps thewindings 30 a and 30 b, the winding 30 c overlaps the winding 30 a and its adjacent inner winding (not shown), and the winding 30 e overlaps the winding 30 b and its adjacent inner winding (not shown), and so on. Thestrip 30 is wound in this manner for length of the 10 or 10′, and it is understood that the number of radially spaced windings, and therefore the thickness of the layer thus formed can vary.pipes - According to the embodiment of
FIG. 3B , acontinuous metal strip 34, preferably of carbon steel, is helically wrapped around the adjacent inner member (not shown). Thestrip 34 is shaped, or formed, in any known manner to form a cross section having a first substantially horizontal inner portion 34 a, and second substantiallyhorizontal portion 34 b that is spaced radially outwardly from the inner portion 34 a, and abent portion 34 c extending between theportions 34 a and 34 b. Thestrip 34 is preferably of carbon steel and is helically wrapped around the adjacent inner member (not shown). The wrapping of thestrip 34 is such that theportion 34 b overlaps the inner portion of its adjacent winding, and the portion 34 a is overlapped by the outer portion of its adjacent winding, to thus achieve an interlocking effect. Thestrip 34 is wrapped for the length of the 10 or 10′, and it is understood that the number of radially spaced windings, and therefore the thickness of the layer thus formed can vary.pipes - According to the embodiment of
FIG. 3C , a continuous metal strip 38, preferably of carobon steel, is helically wrapped around the adjacent inner member (now shown). The strip 38 is shaped, or formed, in any known manner to form a cross section having a convex portion 38 a extending from aconcave portion 38 b. The wrapping of the strip 38 is such that the convex portion 38 a overlaps the concave portion of its adjacent winding and the concave portion 38 a is overlapped by the convex portion of its adjacent winding to thus achieve an interlocking effect. The strip 38 is wrapped for the length of the 10 or 10, and it is understood that the number of radially spaced windings, and therefore the thickness of the layer thus formed can vary.pipes - 1. In each of the above embodiments, additional tensile layers of wires can be provided in addition to the series of
wires 16 a and 16 b in thepipe 10 and the series ofwires 26 a and 26 b inpipe 10′. - 2. The carbon
steel strip layer 14 can be omitted from each of the above embodiments in which case the first tensile layer 16 a would be wound directly onto thesheath 12. - 3. If the carbon steel strip is omitted, as discussed in paragraph 2, above, an optional wrapped tape, similar to the
tape 18 could be provided that extends between thesheath 12 and the first tensile layer 16 a. - 4. The adjacent windings of the strip forming the
layer 14 do not have to be interlocked. - 5. In extremely hostile environments, an outer layer similar to the
layer 14 can be placed around thesheath 20 for added protection, in each of the embodiments. - 6. In extremely hostile environments, an outer layer similar to the
layer 14 can be placed around thesheath 20 for added protection. - It is understood that spatial references, such as “under”, “over”, “between”, “outer”, “inner” and “surrounding” are for the purpose of illustration only and do not limit the specific orientation or location of the layers described above.
- Since other modifications, changes, and substitutions are intended in the foregoing disclosure, it is appropriate that the appended claims be construed broadly and in a manner consistent with the scope of the invention.
Claims (20)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/400,617 US20060191311A1 (en) | 1999-11-05 | 2006-04-06 | Flexible pipe and method of manufacturing same |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16390899P | 1999-11-05 | 1999-11-05 | |
| US70607000A | 2000-11-03 | 2000-11-03 | |
| US10/165,870 US7055551B2 (en) | 1999-11-05 | 2002-06-10 | Flexible pipe and method of manufacturing same |
| US11/400,617 US20060191311A1 (en) | 1999-11-05 | 2006-04-06 | Flexible pipe and method of manufacturing same |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/165,870 Continuation US7055551B2 (en) | 1999-11-05 | 2002-06-10 | Flexible pipe and method of manufacturing same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20060191311A1 true US20060191311A1 (en) | 2006-08-31 |
Family
ID=26860063
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/165,870 Expired - Lifetime US7055551B2 (en) | 1999-11-05 | 2002-06-10 | Flexible pipe and method of manufacturing same |
| US11/400,617 Abandoned US20060191311A1 (en) | 1999-11-05 | 2006-04-06 | Flexible pipe and method of manufacturing same |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/165,870 Expired - Lifetime US7055551B2 (en) | 1999-11-05 | 2002-06-10 | Flexible pipe and method of manufacturing same |
Country Status (5)
| Country | Link |
|---|---|
| US (2) | US7055551B2 (en) |
| EP (2) | EP1975492A3 (en) |
| CN (1) | CN1420973A (en) |
| AU (1) | AU780180B2 (en) |
| WO (1) | WO2001033129A1 (en) |
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| WO2010107995A3 (en) * | 2009-03-18 | 2011-01-13 | Deepflex Inc. | Composite flexible pipe and method of manufacture |
| US20110146366A1 (en) * | 2009-06-19 | 2011-06-23 | Bergrohr Gmbh Siegen | Production-optimized process for producing a multilayer pipe |
| US20110226374A1 (en) * | 2010-03-17 | 2011-09-22 | Deepflex Inc. | Anti-extrusion layer with non-interlocked gap controlled hoop strength layer |
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| US6701969B2 (en) | 2001-10-31 | 2004-03-09 | Wellstream International Limited | Flexible tubular pipe and method of manufacturing same |
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| US4275491A (en) * | 1977-02-08 | 1981-06-30 | Roberto Marinucci | Multi-complex shear device for splitting hot metallic bars into several smaller bars |
| US4285534A (en) * | 1979-12-28 | 1981-08-25 | Nichirin Rubber Industrial Co., Ltd. | Pulsation-absorbing flexible pipe for pressure fluid device |
| US4344462A (en) * | 1979-05-30 | 1982-08-17 | Coflexip | Flexible tubular conduit |
| US4403631A (en) * | 1981-05-12 | 1983-09-13 | Abdullaev Gasan M B O | Flexible pipe |
| US4549581A (en) * | 1984-03-20 | 1985-10-29 | The Furukawa Electric Co., Ltd. | Flexible pipe |
| US4706713A (en) * | 1984-06-20 | 1987-11-17 | Furukawa Electric Co., Ltd. | Flexible composite pipe for high-temperature fluids |
| US4903735A (en) * | 1985-06-11 | 1990-02-27 | Institut Francais Du Petrole | Pipe usable particularly for transporting fluids and allowing the permeability to the fluids transported to be limited |
| US5174685A (en) * | 1992-03-18 | 1992-12-29 | Buchanan Luther B | Flexible pipe laying and covering apparatus |
| US5314210A (en) * | 1990-02-02 | 1994-05-24 | Etablissements Caillau | Device for connecting a flexible pipe to a rigid tubular joining piece |
| US5406984A (en) * | 1988-05-09 | 1995-04-18 | Institut Francais Du Petrole | Hose including an aluminum alloy |
| US5579809A (en) * | 1992-12-08 | 1996-12-03 | Royal Ordnance Plc | Reinforced composite pipe construction |
| US5626044A (en) * | 1995-05-19 | 1997-05-06 | Lara-Castro; Manuel | Method of producing steel bars from billets |
| US5638714A (en) * | 1994-04-20 | 1997-06-17 | Fintube Limited Partnership | Process for making a strip from a rod |
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| US5782506A (en) * | 1995-04-04 | 1998-07-21 | Sanco Co., Ltd. | Flexible pipe |
| US5837083A (en) * | 1993-08-12 | 1998-11-17 | Booth; John Peter | Method of forming a rigid tubular body |
| US5890960A (en) * | 1997-08-29 | 1999-04-06 | Randall H. Fisher | Venting system for structures using a ridge vent |
| US5918641A (en) * | 1990-06-18 | 1999-07-06 | Hardy; Jean | Flexible tubular conduit comprising a jacket made of crosslinked polyethylene device and process for manufacturing such a conduit |
| US5921285A (en) * | 1995-09-28 | 1999-07-13 | Fiberspar Spoolable Products, Inc. | Composite spoolable tube |
| US5934332A (en) * | 1993-10-05 | 1999-08-10 | Angus Fire Armour Limited | Pipe lining |
| US5934335A (en) * | 1995-03-29 | 1999-08-10 | Coflexip Sa | Flexible tubular pipe with an internal impervious polymeric sheath |
| US6004639A (en) * | 1997-10-10 | 1999-12-21 | Fiberspar Spoolable Products, Inc. | Composite spoolable tube with sensor |
| US6016845A (en) * | 1995-09-28 | 2000-01-25 | Fiber Spar And Tube Corporation | Composite spoolable tube |
| US6016847A (en) * | 1989-11-21 | 2000-01-25 | Coflexip | Flexible tubular conduit |
| US6016848A (en) * | 1996-07-16 | 2000-01-25 | W. L. Gore & Associates, Inc. | Fluoropolymer tubes and methods of making same |
| US6053213A (en) * | 1998-02-18 | 2000-04-25 | Coflexip | Flexible pipe for great depths |
| US6098667A (en) * | 1997-09-18 | 2000-08-08 | Institut Francais Du Petrole | Flexible piping structure having a continuous metal inner tube |
| US6123114A (en) * | 1998-02-18 | 2000-09-26 | Coflexip | Flexible pipe for riser in off-shore oil production |
| US20010015233A1 (en) * | 1998-05-28 | 2001-08-23 | Donaldson Company, Inc. | Flexible hose and method for manufacturing |
| US6338365B1 (en) * | 1997-09-18 | 2002-01-15 | Institut Francais Du Petrole | Flexible piping structure having a continuous metal inner tube |
| US6390141B1 (en) * | 1998-12-21 | 2002-05-21 | Parker-Hannifin Corporation | Collapse-resistant hose construction |
| US6408891B1 (en) * | 1998-02-18 | 2002-06-25 | Institut Francais Du Petrole | Flexible pipe for static use in a corrosive ambience |
| US6460389B1 (en) * | 1999-07-29 | 2002-10-08 | Kocks Technik Gmbh & Co. | Method and apparatus for rolling of heated metallic products |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5645109A (en) * | 1990-06-29 | 1997-07-08 | Coflexip | Flexible tubular pipe comprising an interlocked armoring web and process for producing it |
| FR2665237B1 (en) * | 1990-07-27 | 1992-11-13 | Coflexip | FLEXIBLE TUBULAR CARCASS AND CONDUIT COMPRISING SUCH A CARCASS. |
-
2000
- 2000-11-04 EP EP08156860A patent/EP1975492A3/en not_active Withdrawn
- 2000-11-04 CN CN00818233.7A patent/CN1420973A/en active Pending
- 2000-11-04 EP EP00978374A patent/EP1232358A4/en not_active Ceased
- 2000-11-04 WO PCT/US2000/030464 patent/WO2001033129A1/en not_active Ceased
- 2000-11-04 AU AU15845/01A patent/AU780180B2/en not_active Expired
-
2002
- 2002-06-10 US US10/165,870 patent/US7055551B2/en not_active Expired - Lifetime
-
2006
- 2006-04-06 US US11/400,617 patent/US20060191311A1/en not_active Abandoned
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| US4275491A (en) * | 1977-02-08 | 1981-06-30 | Roberto Marinucci | Multi-complex shear device for splitting hot metallic bars into several smaller bars |
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| US5406984A (en) * | 1988-05-09 | 1995-04-18 | Institut Francais Du Petrole | Hose including an aluminum alloy |
| US6016847A (en) * | 1989-11-21 | 2000-01-25 | Coflexip | Flexible tubular conduit |
| US5314210A (en) * | 1990-02-02 | 1994-05-24 | Etablissements Caillau | Device for connecting a flexible pipe to a rigid tubular joining piece |
| US5918641A (en) * | 1990-06-18 | 1999-07-06 | Hardy; Jean | Flexible tubular conduit comprising a jacket made of crosslinked polyethylene device and process for manufacturing such a conduit |
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| US5174685A (en) * | 1992-03-18 | 1992-12-29 | Buchanan Luther B | Flexible pipe laying and covering apparatus |
| US5579809A (en) * | 1992-12-08 | 1996-12-03 | Royal Ordnance Plc | Reinforced composite pipe construction |
| US5837083A (en) * | 1993-08-12 | 1998-11-17 | Booth; John Peter | Method of forming a rigid tubular body |
| US5934332A (en) * | 1993-10-05 | 1999-08-10 | Angus Fire Armour Limited | Pipe lining |
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| US5934335A (en) * | 1995-03-29 | 1999-08-10 | Coflexip Sa | Flexible tubular pipe with an internal impervious polymeric sheath |
| US5782506A (en) * | 1995-04-04 | 1998-07-21 | Sanco Co., Ltd. | Flexible pipe |
| US5626044A (en) * | 1995-05-19 | 1997-05-06 | Lara-Castro; Manuel | Method of producing steel bars from billets |
| US5676175A (en) * | 1995-06-26 | 1997-10-14 | Golan Plastic Products | Plastic liner |
| US6016845A (en) * | 1995-09-28 | 2000-01-25 | Fiber Spar And Tube Corporation | Composite spoolable tube |
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| US6016848A (en) * | 1996-07-16 | 2000-01-25 | W. L. Gore & Associates, Inc. | Fluoropolymer tubes and methods of making same |
| US5730188A (en) * | 1996-10-11 | 1998-03-24 | Wellstream, Inc. | Flexible conduit |
| US5890960A (en) * | 1997-08-29 | 1999-04-06 | Randall H. Fisher | Venting system for structures using a ridge vent |
| US6098667A (en) * | 1997-09-18 | 2000-08-08 | Institut Francais Du Petrole | Flexible piping structure having a continuous metal inner tube |
| US6338365B1 (en) * | 1997-09-18 | 2002-01-15 | Institut Francais Du Petrole | Flexible piping structure having a continuous metal inner tube |
| US6004639A (en) * | 1997-10-10 | 1999-12-21 | Fiberspar Spoolable Products, Inc. | Composite spoolable tube with sensor |
| US6053213A (en) * | 1998-02-18 | 2000-04-25 | Coflexip | Flexible pipe for great depths |
| US6123114A (en) * | 1998-02-18 | 2000-09-26 | Coflexip | Flexible pipe for riser in off-shore oil production |
| US6408891B1 (en) * | 1998-02-18 | 2002-06-25 | Institut Francais Du Petrole | Flexible pipe for static use in a corrosive ambience |
| US20010015233A1 (en) * | 1998-05-28 | 2001-08-23 | Donaldson Company, Inc. | Flexible hose and method for manufacturing |
| US6390141B1 (en) * | 1998-12-21 | 2002-05-21 | Parker-Hannifin Corporation | Collapse-resistant hose construction |
| US6460389B1 (en) * | 1999-07-29 | 2002-10-08 | Kocks Technik Gmbh & Co. | Method and apparatus for rolling of heated metallic products |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010107995A3 (en) * | 2009-03-18 | 2011-01-13 | Deepflex Inc. | Composite flexible pipe and method of manufacture |
| US8656961B2 (en) | 2009-03-18 | 2014-02-25 | Deepflex Inc. | Composite flexible pipe and method of manufacture |
| US20110146366A1 (en) * | 2009-06-19 | 2011-06-23 | Bergrohr Gmbh Siegen | Production-optimized process for producing a multilayer pipe |
| US20110226374A1 (en) * | 2010-03-17 | 2011-09-22 | Deepflex Inc. | Anti-extrusion layer with non-interlocked gap controlled hoop strength layer |
| US8967205B2 (en) * | 2010-03-17 | 2015-03-03 | Deepflex Inc. | Anti-extrusion layer with non-interlocked gap controlled hoop strength layer |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1975492A3 (en) | 2009-07-01 |
| US7055551B2 (en) | 2006-06-06 |
| EP1232358A1 (en) | 2002-08-21 |
| WO2001033129A1 (en) | 2001-05-10 |
| AU1584501A (en) | 2001-05-14 |
| AU780180B2 (en) | 2005-03-03 |
| US20020144745A1 (en) | 2002-10-10 |
| EP1975492A2 (en) | 2008-10-01 |
| CN1420973A (en) | 2003-05-28 |
| EP1232358A4 (en) | 2004-06-02 |
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| AS | Assignment |
Owner name: WELLSTREAM INTERNATIONAL LIMITED, UNITED KINGDOM Free format text: CHANGE OF NAME;ASSIGNOR:BLOSSOMGRANGE LIMITED;REEL/FRAME:018278/0613 Effective date: 20030312 Owner name: BLOSSOMGRANGE LIMITED, UNITED KINGDOM Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:WELLSTREAM, INC.;REEL/FRAME:018278/0605 Effective date: 20030310 Owner name: WELLSTREAM, INC., FLORIDA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:FRASER, DANA J.;HOEFLING, ROBERT G.;KALMAN, MARK D.;AND OTHERS;REEL/FRAME:018278/0489;SIGNING DATES FROM 20010307 TO 20010308 |
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| AS | Assignment |
Owner name: THE GOVERNOR AND COMPANY OF THE BANK OF SCOTLAND, Free format text: SECURITY AGREEMENT;ASSIGNOR:WELLSTREAM INTERNATIONAL LIMITED;REEL/FRAME:019235/0499 Effective date: 20070501 |
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| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |