IP Library Granted Patent US 10,030,793
Granted Patent B2
US 10,030,793 · App. 14/000,268 · Granted Jul 24, 2018

Flexible pipe body and method of producing same

Inventor: Neville Dodds (Tyne and Wear, GB)
Assignee: GE Oil & Gas UK Limited
F16L11/00B29C53/582B29C53/64B29D23/001F16L11/081B29C61/006B29C63/10B29K2105/243F16L2011/047
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Quick Facts
Patent No.
US 10,030,793
App. No.
14/000,268
Granted
Jul 24, 2018
Kind
B2
Abstract

To produce a flexible pipe body, a length of tensile armour element ( 300 ) of pre-preg composite material is fed towards a fluid-retaining layer ( 602 ). The tensile armour element ( 300 ) passes through a guide ( 604 ) an a pre-heater ( 606 ). The tensile armour element ( 300 ) is then applied to the fluid-retaining layer ( 602 ), being wrapped around the fluid-etaining layer ( 602 ) by virtue of the rotation of the layer ( 602 ), the linear translation of the layer ( 602 ), and the fixed position of the tensile armour element feed ( 601 ). The element ( 300 ) is fed to the fluid-retaining layer under a constant, predetermined controlled tension. Positioning head ( 608 ) helps to position the element ( 300 ) on the fluid-retaining layer ( 602 ). As tensile armour element is wound onto the pipe body, the pipe body continues to move in a, linear direction and the pipe body moves through an oven ( 610 ).

Claims (25)

1. A method of producing a flexible pipe body for transporting production fluids from a sub-sea location, the method comprising:

providing a plurality of lengths of a thermosetting composite material and stacking the plurality of lengths of the thermosetting composite material to form a tensile armour element;

applying a heat-shrink tape or a heat-shrink sleeve to the plurality of lengths of the thermosetting composite material;

helically wrapping the tensile armour element, under a predetermined tension, around a fluid-retaining layer; and

then heating the tensile armour element to cure the thermosetting composite material and form a bond between the stacked lengths of the thermosetting composite material while preventing neighboring elements of the tensile armour element from bonding together during the curing process;

wherein the tensile armour element forms a structural armour layer, and said armour layer comprises a lay angle in a range of about 10° to about 55°.

2. The method as in claim 1 , wherein the thermosetting composite material comprises a thermosetting matrix material and a plurality of reinforcing fibers.

3. The method as in claim 2 , wherein more than 50% of the plurality of reinforcing fibers are aligned in a direction substantially axially with the length of the material.

4. The method as in claim 1 , wherein the thermosetting composite material is substantially free from residual strain.

5. The method as in claim 1 , wherein the predetermined tension is in the range of 100 N to 1000 N.

6. The method as in claim 1 , wherein helically wrapping the tensile armour element comprises helically wrapping the length such that adjacent sections of the thermosetting composite material helically wrapped around the fluid-retaining layer do not overlap.

7. The method as in claim 1 , wherein helically wrapping the tensile armour element comprises helically wrapping the length such that adjacent sections of the thermosetting composite material helically wrapped around the fluid-retaining layer at least partially overlap.

8. The method as in claim 1 , wherein the heat-shrink tape or the heat-shrink sleeve comprises a low friction material.

9. A flexible pipe body for transporting production fluids from a sub-sea location, comprising:

a fluid-retaining layer; and

at least one structural armour layer comprising a tensile armour element comprising a plurality of stacked lengths of thermosetting composite material, provided over the fluid-retaining layer, and further comprising a heat-shrink tape or a heat-shrink sleeve over the plurality of stacked lengths of thermostetting composite material;

wherein the armour layer is formed by helically wrapping the tensile armour element, under a predetermined tension, around the fluid-retaining layer and then heating the tensile armour element to cure the thermosetting material and forming a bond between the stacked lengths of the thermosetting material; and

wherein said armour layer has a lay angle in a range of about 10° to about 55°.

10. The flexible pipe body as in claim 9 , wherein the thermosetting composite material comprises a thermosetting matrix material and a plurality of reinforcing fibers.

11. The flexible pipe body as in claim 10 , wherein more than 50% of the plurality of reinforcing fibers are aligned in a direction substantially axially with the length of the material.

12. The flexible pipe body as in claim 9 , wherein the armour layer is substantially free from residual strain.

13. The flexible pipe body as in claim 9 , wherein the predetermined tension is in the range of 100 N to 1000 N.

14. The flexible pipe body as in claim 9 , wherein adjacent sections of the thermosetting composite material helically wrapped over the fluid-retaining layer do not overlap with the armour layer.

15. The flexible pipe body as in claim 9 , wherein adjacent sections of the thermosetting composite material helically wrapped over the fluid-retaining layer at least partially overlap with the armour layer.

16. The flexible pipe body as in claim 9 , wherein the heat-shrink tape or heat-shrink sleeve comprises a low friction material.

Assignments (3)
CHANGE OF NAME Recorded Sep 25, 2024
From: GE OIL & GAS UK LIMITED
To: BAKER HUGHES ENERGY TECHNOLOGY UK LIMITED
Reel/Frame 068687/0506 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 17, 2014
From: WELLSTREAM INTERNATIONAL LIMITED
To: GE OIL & GAS UK LIMITED
Reel/Frame 034013/0657 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 28, 2013
From: DODDS, NEVILLE
To: WELLSTREAM INTERNATIONAL LIMITED
Reel/Frame 031486/0823 →
Priority Claims (1)
GB 1105067.1 · Mar 25, 2011 · national
Continuity (1)
Related Publication 20140007970A1 · Jan 9, 2014
Cited By (1)
US 12,247,686