Composite pressure vessel assembly and method of manufacturing

Patent metadata

Field	Value
Publication number	US-10907768-B2
Application number	US-201616095570-A
Country	US
Kind code	B2
Filing date	Apr 22, 2016
Priority date	Apr 22, 2016
Publication date	Feb 2, 2021
Grant date	Feb 2, 2021

Abstract

A composite pressure vessel assembly includes a first vessel having a first inner layer and a second vessel having a second inner layer. An outer layer of the assembly is in contact with and substantially envelopes the first and second inner layers. A junction of the assembly has outer boundaries defined by segments of the first inner layer, the second inner layer and the outer layer. A cross-layered component of the assembly is disposed in the junction, the first and second inner layers and the outer layer for adding strength to the junction and restricting delamination.

First claim

What is claimed is:

1. A composite pressure vessel assembly comprising:
a first vessel including a first inner layer;
a second vessel including a second inner layer;
an outer layer being in contact with and substantially enveloping the first and second inner layers;
a junction having outer boundaries defined by segments of the first inner layer, the second inner layer and the outer layer; and
a cross-layered component disposed in-part in and projecting through the junction, and disposed in-part in the first and second inner layers and the outer layer, wherein the cross-layered component is a plurality of stitchings adapted to engage the outer layer with at least one of the adjacent first and second inner layers.

2. The composite pressure vessel assembly set forth in claim 1 , wherein the first vessel includes a first liner defining a first chamber and the first inner layer substantially envelopes the first liner, and wherein the second vessel includes a second liner defining a second chamber and the second layer substantially envelopes the second liner, and wherein the plurality of stitchings do not project into the first and second liners.

3. The composite pressure vessel assembly set forth in claim 2 , wherein the first and second vessels are aligned side-by-side with a portion of the first inner layer in contact with a portion of the second inner layer.

4. The composite pressure vessel assembly set forth in claim 3 , wherein the portions and segments of the first and second inner layers are not in direct contact with the outer layer.

5. The composite pressure vessel assembly set forth in claim 4 , wherein the first and second liners are made of a formable polymer material.

6. The composite pressure vessel assembly set forth in claim 4 , wherein the first and second liners are metallic.

7. The composite pressure vessel assembly set forth in claim 1 , wherein the junction is generally centered to a Y-shaped seam.

8. The composite pressure vessel assembly set forth in claim 7 , wherein the junction is made of the same material as the outer layer.

9. The composite pressure vessel assembly set forth in claim 1 , wherein the cross-layered component includes a plurality of rods.

10. The composite pressure vessel assembly set forth in claim 9 , wherein at least a portion of the plurality of rods extend through the outer layer, the junction, and into at least one of the first and second inner layers.

11. The composite pressure vessel assembly set forth in claim 10 , wherein at least a portion of the plurality of rods extend through the outer layer and into the first inner layer.

12. The composite pressure vessel assembly set forth in claim 1 , wherein the first and second inner layers are made of a generally continuous fiber, and the outer layer is made of a random fiber fabric.

13. The composite pressure vessel assembly set forth in claim 1 , wherein the first and second inner layers are made of a generally continuous fiber, and the outer layer is made of a weaved fiber fabric.

14. The composite pressure vessel assembly set forth in claim 9 , wherein the first and second inner layers and the outer layer form a prepreg laminate when the rods are inserted into the laminate.

15. A composite pressure vessel assembly comprising,
a first vessel including a first inner layer;
a second vessel including a second inner layer;
an outer layer being in contact with and substantially enveloping the first and second inner layers;
a junction having outer boundaries defined by segments of the first inner layer, the second inner layer and the outer layer; and
a cross-layered component disposed in-part in the junction, disposed in-part in the first and second inner layers and disposed in-part in the outer layer, wherein the cross-layered component is an inter-weave disposed between the outer layer and at least one of the first and second inner layers.

16. A method of manufacturing a composite pressure vessel assembly comprising:
enveloping a first liner with a first fiber composite layer;
enveloping a second liner with a second fiber composite layer;
placing the first and second liners side-by-side such that portions of the at least first and second fiber composite layers are in contact with one-another;
enveloping the first and second fiber composite layers with a third fiber composite layer; and
applying a cross-layered component generally at junctions of the pressure vessel defined by segments of the first, second, and third fiber composite layers, wherein the cross-layered component is a plurality of stitchings adapted to engage the outer layer with at least one of the adjacent first and second inner layers, and the plurality of stitchings do not extend into the first and second fiber composite layers.

17. The method set forth in claim 16 further comprising:
curing a resin of the first, second, and third fiber composite layers after applying the cross-layered component.

18. The method set forth in claim 17 , wherein the cross-layered component is Z-pins.

19. The method set forth in claim 17 , wherein the plurality of stitchings are an inter-weave of fibers between the third fiber composite layer and at least one of the first and second fiber composite layers.

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Zhao Wenping
• Sun Ellen Y
• Croteau Paul F
• Hawkes Justin R
• Kuczek Andrzej Ernest

Classifications

• F17C1/04 Primary

  Protecting sheathings · CPC title

• B29D22/003 Primary

  Containers for packaging, storing or transporting, e.g. bottles, jars, cans, barrels, tanks · CPC title

• B29D99/0005

  Producing noodles, i.e. composite gap fillers, characterised by their construction · CPC title

• F17C2260/018

  Adapting dimensions · CPC title

• F17C2223/036

  Very high pressure (>80 bar) · CPC title