Method of making a device for controlling stress in joints at cryogenic temperatures

Patent metadata

Field	Value
Publication number	US-10399709-B2
Application number	US-201213541534-A
Country	US
Kind code	B2
Filing date	Jul 3, 2012
Priority date	Jul 18, 2008
Publication date	Sep 3, 2019
Grant date	Sep 3, 2019

Abstract

A composite resin tank includes a wall joined to a dome along a joint. A softening strip is used to control stress in the joint.

First claim

The invention claimed is:

1. A method of making a softening strip for controlling stress in a joint, comprising:
producing a fabric preform having fibers extending in three dimensions, wherein the fibers are arranged along three substantially orthogonal axes and are evenly distributed throughout the fabric preform to form a grid of fibers extending in three dimensions and having intersections such that three or more of the fibers intersect at any given intersection of the intersections, wherein each intersecting fiber has a single point of contact with each other intersecting fiber at any given intersection; and
coating surfaces of the fibers with a thermoplastic polymer binder, wherein the thermoplastic polymer binder encapsulates each intersection to form a unified junction of fibers.

2. The method of claim 1 , wherein coating surfaces of the fibers includes:
preparing an aqueous solution containing particles of the thermoplastic polymer binder,
immersing the fabric preform in the aqueous solution to form an infused fabric, and
adhering the particles of the thermoplastic polymer binder to the surfaces of the fibers by drying the infused fabric.

3. The method of claim 2 , wherein coating surfaces of the fibers includes:
placing the infused fabric in a vacuum, and
using the vacuum to draw air bubbles from the aqueous solution.

4. The method of claim 2 , wherein coating surfaces of the fibers includes heating the particles of the thermoplastic polymer binder adhered to the fibers until the particles of the thermoplastic polymer binder melt and flow together around the fibers.

5. The method of claim 4 , wherein the heating includes heating the particles of the thermoplastic polymer binder to a temperature of at least 500° F.

6. The method of claim 1 , wherein coating surfaces of the fibers includes:
adhering binder particles to the surfaces of the fibers, and
sintering the binder particles.

7. The method of claim 1 , further comprising:
loosening bonds between the coated surfaces of the fibers by cold working the fabric preform.

8. The method of claim 7 , wherein cold working the fabric preform is performed by one of:
passing the fabric preform through and compressing the fabric preform between a pair of rollers, and
pressing the fabric preform between two dies.

9. The method of claim 7 , further comprising shaping the fabric preform as the bonds between the coated surfaces of the fibers are being loosened.

10. The method of claim 7 , further comprising:
machining the fabric preform with the coated surfaces of the fibers to a desired
shape related to the joint.

11. The method of claim 6 , wherein the fabric preform includes one of:
woven fibers,
braided fibers,
stacked layers of fibers,
stitched fibers, and
pinned layers of fibers.

12. The method of claim 6 , wherein the fibers are selected from the group consisting of:
graphite fibers,
glass fibers, and
aramid fibers.

13. The method of claim 6 , wherein:
the fibers include fibers extending along three substantially orthogonal axes, and
the fabric preform has a shape matching the joint and is in face-to-face contact with each of the surfaces.

14. The method of claim 6 , wherein the fibers include fibers having a diameter within a range of 2 to 15 microns.

15. The method of claim 6 , wherein the thermoplastic polymer binder is a polymer that is compliant at both room temperature and at cryogenic temperatures.

16. The method of claim 6 , wherein:
the thermoplastic polymer binder is a fluoropolymer exhibiting flexibility at temperatures below −150° F. and stability at temperatures up to 400° F., and
the fibers are graphite fibers.

17. The method of claim 6 , wherein the fabric preform is porous and is flexible at cryogenic temperatures.

18. The method of claim 6 , wherein the fibers and the thermoplastic polymer binder are flexible at cryogenic temperatures.

19. A method of manufacturing a structural assembly, comprising:
forming a first composite resin structure having a first surface;
forming a second composite resin structure having a second surface;
forming a joint between the first and second surfaces, wherein the joint connects the first and second surfaces; and
forming a softening strip in the joint for controlling stress in the joint, wherein forming the softening strip further comprises:
producing a fabric preform having fibers extending in three dimensions, wherein the fibers are arranged along three substantially orthogonal axes and are evenly distributed throughout the fabric preform to form a grid of fibers extending in three dimensions and having intersections such that three or more of the fibers intersect at any given intersection of the intersections, wherein each intersecting fiber has a single point of contact with each other intersecting fiber at any given intersection; and
coating surfaces of the fibers with a thermoplastic polymer binder, wherein the thermoplastic polymer binder encapsulates each intersection to form a unified junction of fibers.

20. The method of claim 19 , wherein the joint is Y-shaped and the softening strip is wedge shaped, and wherein the method further comprises:
placing the softening strip in face-to-face contact with the first and second surfaces.

21. The method of claim 20 , further comprising:
linearizing, using the softening strip, the stress in the joint at cryogenic temperatures.

22. The method of claim 20 , wherein the thermoplastic polymer binder has a melting point higher than a temperature required to cure the first and second composite resin structures.

23. The method of claim 19 wherein:
producing the fabric preform having fibers extending in three dimensions comprises arranging the fibers along substantially orthogonal axes in a generally proportional and evenly distributed manner throughout the fabric preform, such that the orthogonal fibers intersect and contact each other at intersections; and
coating surfaces of the fibers with a thermoplastic polymer binder comprises surrounding the fibers and encapsulating multiple fibers at the intersections, such that spacings between the fibers remain, whereby porosities are provided in the fabric preform.

24. A method of making a softening strip for controlling stress in a joint, comprising:
producing a fabric preform having fibers extending in three dimensions, including:
arranging a first plurality of fibers in parallel along a first longitudinal axis;
arranging a second plurality of fibers in parallel along a second longitudinal axis orthogonal to the first longitudinal axis, wherein the second plurality of fibers intersects the first plurality of fibers;
arranging a third plurality of fibers in parallel along a third longitudinal axis orthogonal to the first and second longitudinal axes, wherein the third plurality of fibers intersects the first and second pluralities of fibers;
wherein the orthogonal fibers intersect and contact each other at intersections in an evenly distributed manner throughout the fabric preform, and wherein each intersection includes at least three fibers arranged along corresponding ones of the three orthogonal axes, wherein each intersecting fiber has a single point of contact with each other intersecting fiber at any given intersection; and

coating surfaces of the fibers with a thermoplastic polymer binder, wherein the thermoplastic polymer binder encapsulates each intersection to form a

Assignees

• Robinson Michael J
• Hand Michael Leslie
• Blevins Creed Ernest
• Boeing Co

Inventors

• Robinson Michael J
• Hand Michael Leslie
• Blevins Creed Ernest

Classifications

• B64G1/64 Primary

  Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements · CPC title

• B64G1/66

  Arrangements or adaptations of apparatus or instruments, not otherwise provided for · CPC title

• Y10T442/20

  Coated or impregnated woven, knit, or nonwoven fabric which is not [a] associated with another preformed layer or fiber layer or, [b] with respect to woven and knit, characterized, respectively, by a particular or differential weave or knit, wherein the coating or impregnation is neither a foamed material nor a free metal or alloy layer · CPC title

• Y10T442/2631

  Coating or impregnation provides heat or fire protection · CPC title

• Y10T442/2008

  Fabric composed of a fiber or strand which is of specific structural definition · CPC title