Mold-less curing method of manufacturing a composite vessel assembly

Patent metadata

Field	Value
Publication number	US-10913210-B2
Application number	US-201715440448-A
Country	US
Kind code	B2
Filing date	Feb 23, 2017
Priority date	Feb 23, 2017
Publication date	Feb 9, 2021
Grant date	Feb 9, 2021

Abstract

A method of manufacturing a composite vessel assembly includes the step of placing the composite vessel assembly in a pliable containment prior to curing of a resin of the composite vessel assembly. With the composite vessel assembly in the pliable containment, a vacuum is applied through an orifice in the pliable containment to evacuate air and compact the composite vessel assembly.

First claim

What is claimed is:

1. A method of manufacturing a composite vessel assembly comprising:
placing the composite vessel assembly in a pliable containment prior to curing of a resin of the composite vessel assembly; and
applying a vacuum to the inside of the pliable containment and through a first orifice in a pliable portion of the pliable containment to evacuate air and compact the composite vessel assembly.

2. The method set forth in claim 1 , wherein the pliable containment is in biased contact with the composite vessel assembly when the vacuum is applied, and the pliable containment is completely pliable.

3. The method set forth in claim 1 , further comprising:
sealing a portion of the pliable containment that defines a second orifice about a nozzle of the composite vessel assembly; and
placing a chamber of the composite vessel assembly under a pressure equal to or greater than atmospheric pressure when the pliable containment is under the vacuum.

4. The method set forth in claim 3 , wherein a liner of the composite vessel assembly defines the chamber and a composite layer of the composite vessel assembly at least in-part surrounds the liner.

5. The method set forth in claim 1 further comprising:
curing the resin of the composite vessel assembly when under the vacuum.

6. The method set forth in claim 5 , further comprising:
wrapping the composite vessel assembly with at least one sheet before placing the composite vessel assembly in the pliable containment;
releasing the vacuum after the resin has cured;
removing the composite vessel assembly and the at least one sheet from the pliable containment; and
removing the at least one sheet from the composite vessel assembly.

7. The method set forth in claim 1 , further comprising:
drawing the uncured resin when in a fluid state into the pliable containment and through a third orifice in the pliable containment when under the vacuum; and
infusing the composite vessel assembly with the uncured resin.

8. The method set forth in claim 1 , wherein the pliable containment is a bag.

9. The method set forth in claim 1 , further comprising:
wrapping the composite vessel assembly with at least one sheet before placing the composite vessel assembly in the pliable containment;
releasing the vacuum;
removing the composite vessel assembly and the at least one sheet from the pliable containment; and
removing the at least one sheet from the composite vessel assembly.

10. The method set forth in claim 9 , wherein the at least one sheet includes a porous release film.

11. The method set forth in claim 1 , further comprising:
filling a chamber defined by a liner of the composite vessel assembly with a granulate.

12. The method set forth in claim 11 , further comprising:
plugging a nozzle of the composite vessel assembly after filling the chamber with the granulate and before applying the vacuum.

13. The method set forth in claim 11 , wherein the liner is at least in part surrounded by a composite layer exposed to the vacuum and in contact with the pliable containment when under the vacuum, and the pliable containment is completely pliable.

14. The method set forth in claim 1 , wherein the composite vessel assembly includes an outer composite layer, a plurality of vessels, and a plurality of junctions generally disposed between each adjacent vessel of the plurality of vessels, and wherein the outer composite layer surrounds the plurality of vessels and the plurality of junctions.

15. The method set forth in claim 14 , wherein the outer composite layer and the plurality of junctions are resin-based and uncured when the vacuum is applied.

16. The method set forth in claim 1 , further comprising:
releasing the vacuum prior to curing of the resin;
removing the composite vessel assembly from the pliable containment; and
placing the composite vessel assembly in a mold for curing of the resin.

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Zhao Wenping
• Sun Ellen Y

Classifications

• F17C2203/0604

  Liners · CPC title

• F17C2203/066

  Plastics · CPC title

• F17C2221/035

  Propane butane, e.g. LPG, GPL · CPC title

• F17C2209/2109

  Moulding · CPC title

• F17C1/04

  Protecting sheathings · CPC title