Method of manufacturing a composite vessel assembly

Patent metadata

Field	Value
Publication number	US-11926109-B2
Application number	US-201616095587-A
Country	US
Kind code	B2
Filing date	Apr 22, 2016
Priority date	Apr 22, 2016
Publication date	Mar 12, 2024
Grant date	Mar 12, 2024

Abstract

A method of manufacturing a composite vessel assembly ( 20 ) includes the steps of filling a first chamber defined by a first liner ( 28,30,32 ) with a first granulated material ( 96 ) through a first orifice ( 98 ) in the first liner. A vacuum is then applied to the first chamber, and the first orifice is plugged. The first liner may then be enveloped with a first layer ( 84 ) for structural rigidity followed by relief of the vacuum.

First claim

What is claimed is:

1. A method of manufacturing a composite vessel assembly comprising: placing a first liner in a first pre-form fixture prior to filling with a first granulated material; filling a first chamber defined by the first liner with the first granulated material through a first orifice in the first liner; applying a vacuum to the first chamber; plugging the first orifice; enveloping the first liner with a first layer for structural rigidity, wherein the first liner lines and is in contact with the first layer, and wherein the first liner is flexible and collapsible without the first layer; curing the first layer before relieving the vacuum from the first chamber; and relieving the vacuum, wherein the first layer adheres to an outer layer of the first liner and maintains a shape of the first liner after the vacuum is relieved, wherein the first layer becomes structurally rigid before relieving the vacuum from the first chamber within the first liner, and wherein the composite vessel is configured to store a pressurized fluid in a cavity formed by an interior surface of the first liner after curing.

2. The method of manufacturing set forth in claim 1 , wherein the vacuum is relieved through the first orifice by unplugging the first orifice.

3. The method of manufacturing set forth in claim 1 further comprising: removing the first liner from the first pre-form fixture before enveloping the liner with the first layer.

4. The method of manufacturing set forth in claim 1 , wherein the first layer is a composite layer.

5. The method of manufacturing set forth in claim 2 further comprising:
removing the first granulated material through the first orifice.

6. The method of manufacturing set forth in claim 5 , wherein removing the first granulated material is performed by dissolving the first granulated material.

7. The method of manufacturing set forth in claim 1 , wherein the first liner is made of a polymer and the first layer is made of a resin impregnated fiber-based material.

8. The method of manufacturing set forth in claim 1 , wherein the first granulated material is a gas absorbent material.

9. The method of manufacturing set forth in claim 1 further comprising:
filling a second chamber defined by a second liner with a second granulated material through a second orifice in the second liner;
applying a vacuum to the second chamber;
plugging the second orifice;
enveloping the second liner with a second layer for structural rigidity;
relieving the vacuum; and
enveloping the first and second layers with a third layer.

10. The method of manufacturing set forth in claim 9 , wherein a portion of the first and second layers are placed in direct contact with one-another before the first and second layers are enveloped by a third layer.

11. The method of manufacturing set forth in claim 9 further comprising:
placing the second liner in a second pre-form fixture prior to filling with the second granulated material.

12. The method of manufacturing set forth in claim 11 further comprising:
removing the second liner from the second pre-form fixture before enveloping with the second layer.

13. The method of manufacturing set forth in claim 10 , wherein the first and second layers are made of a resin-based composite material.

14. The method of manufacturing set forth in claim 13 , wherein the first and second layers are enveloped by the third layer be fore the first and second layers are cured.

15. The method of manufacturing set forth in claim 14 , wherein the third layer is a resin-based composite material.

16. The method of manufacturing set forth in claim 15 further comprising:
removing the first and second granulated materials through the respective first and second orifices.

17. A method of manufacturing a composite vessel assembly comprising: placing a liner in a first pre-form fixture prior to filling with a first granulated material; filling a first chamber defined by liner with granulated material through an orifice in the liner; applying a vacuum to the first chamber; plugging the orifice; enveloping the liner with a layer for structural rigidity, wherein the liner lines and is in contact with the layer, wherein the liner is flexible and collapsible without the layer; curing the layers before relieving the vacuum from the first chamber; and relieving the vacuum, wherein the layer adheres to an outer layer of the liner, and the layer becomes structurally rigid and maintains a shape of the liner, and wherein the composite vessel is configured to store a pressurized fluid in a cavity formed by an interior surface of the liner after curing.

Assignees

• Rtx Corp

Inventors

• Kuczek Andrzej Ernest
• Sun Ellen Y
• Zhao Wenping

Classifications

• B29C70/42 Primary

  for producing articles of definite length, i.e. discrete articles · CPC title

• B29C33/52

  soluble or fusible {(in particular used in injection moulding B29C45/4457)} · CPC title

• B29C33/54

  made of powdered or granular material · CPC title

• B29C70/345

  using matched moulds · CPC title

• B29C70/682

  Preformed parts characterised by their structure, e.g. form · CPC title