Pressure vessel having grooved liner

Patent metadata

Field	Value
Publication number	US-11047530-B2
Application number	US-201816175218-A
Country	US
Kind code	B2
Filing date	Oct 30, 2018
Priority date	Oct 30, 2018
Publication date	Jun 29, 2021
Grant date	Jun 29, 2021

Abstract

Pressure vessels having a grooved liner and methods of forming the same are described. The pressure vessel includes a liner surrounding a cavity therein, an outer surface of the liner disposed opposite the cavity, a boss disposed at a first end of the liner, a composite layer surrounding the liner, an inner surface of the composite layer disposed proximate the liner, and a plurality of longitudinal grooves configured to release gas present between the inner surface of the composite layer and the outer surface of the liner. The liner defines a longitudinal axis therethrough. The boss and the outer surface of the liner define the plurality of longitudinal grooves therein. The plurality of longitudinal grooves extends along the longitudinal axis from the boss toward a second end of the liner. The composite layer spans each of the plurality of longitudinal grooves.

First claim

What is claimed is:

1. A pressure vessel comprising:
a liner surrounding a cavity therein, the liner defining a longitudinal axis therethrough;
an outer surface of the liner disposed opposite the cavity;
a boss disposed at a first end of the liner, the boss being coupled to the liner to form a substantially airtight seal therebetween;
a composite layer surrounding the liner;
an inner surface of the composite layer disposed proximate the liner;
a plurality of longitudinal grooves configured to release gas present between the inner surface of the composite layer and the outer surface of the liner, the boss and the outer surface of the liner defining the plurality of longitudinal grooves therein, the plurality of longitudinal grooves extending along the longitudinal axis from the boss toward a second end of the liner, the composite layer spanning each of the plurality of longitudinal grooves; and
a plurality of inserts, each of the plurality of inserts disposed in a respective one of the plurality of longitudinal grooves;
wherein each of the plurality of inserts is configured to substantially fill the respective one of the plurality of longitudinal grooves in response to a temperature of the plurality of inserts being above a predetermined temperature; and
wherein a conduit is formed between each of the plurality of inserts and the plurality of longitudinal grooves, the conduit providing a passageway in the respective one of the plurality of longitudinal grooves in response to the temperature of the plurality of inserts being less than the predetermined temperature.

2. The pressure vessel of claim 1 , wherein each of the plurality of inserts is formed from materials having a coefficient of thermal expansion that is at least 20% greater than coefficients of thermal expansion of the liner and the composite layer.

3. The pressure vessel of claim 1 , wherein the predetermined temperature corresponds to a curing temperature for the composite layer.

4. The pressure vessel of claim 1 , wherein each of the plurality of inserts is configured to shrink, in response to discharge of pressurized gas stored within the cavity, to thereby release gas between the inner surface of the composite layer and the outer surface of the composite layer through the respective one of the plurality of longitudinal grooves.

5. The pressure vessel of claim 1 , wherein the inserts are configured to define the at least one conduit in response to discharge of pressurized gas stored within the cavity.

6. The pressure vessel of claim 1 , wherein the plurality of inserts are disposed within the longitudinal grooves such that the outer surface of the liner is continuous after pressure equalization and discontinuous in response to discharge of the pressure vessel.

7. A method of forming a pressure vessel, the method comprising:
forming a liner surrounding a cavity therein, the liner defining a longitudinal axis therethrough, the liner including an outer surface disposed opposite the cavity, the liner defining a plurality of first grooves on the outer surface thereof;
obtaining a boss defining a plurality of second grooves;
attaching the boss to a first end of the liner such that each of the plurality of first grooves aligns with a respective one of the plurality of second grooves to thereby form a plurality of longitudinal grooves extending along the longitudinal axis from the boss toward a second end of the liner;
introducing each of a plurality of inserts to a respective one of the plurality of longitudinal grooves;
applying a composite layer to thereby surround the liner, the composite layer spanning each of the plurality of longitudinal grooves; and
curing the composite layer at an elevated temperature such that each of the plurality of inserts substantially fills the respective one of the plurality of longitudinal grooves in response to a temperature of the plurality of inserts being above a predetermined temperature;
wherein a conduit is formed between each of the plurality of inserts and the plurality of longitudinal grooves, the conduit providing a passageway in the respective one of the plurality of longitudinal grooves in response to the temperature of the plurality of inserts being less than the predetermined temperature.

8. The method of claim 7 , further comprising cooling, after curing the composite layer, the pressure vessel and removing the plurality of inserts from the plurality of longitudinal grooves.

9. The method of claim 7 , wherein each of the plurality of inserts is formed from materials having a coefficient of thermal expansion that is at least 20% greater than coefficients of thermal expansion of the liner and the composite layer.

10. The method of claim 7 , wherein each of the plurality of inserts is configured to shrink, in response to discharge of pressurized gas stored within the cavity, to thereby release gas between an inner surface of the composite layer and the outer surface of the liner through the respective one of the plurality of longitudinal grooves.

11. The method of claim 7 , wherein the conduit is defined only during discharge of pressurized gas within the cavity.

12. The method of claim 7 , wherein the plurality of inserts are disposed within the longitudinal grooves such that the outer surface of the liner is continuous after pressure equalization and discontinuous in response to discharge of the pressure vessel.

Assignees

• Gm Global Tech Operations Llc

Inventors

• Beckner Matthew
• Anculle Edward A

Classifications

• Y02E60/32

  Hydrogen storage · CPC title

• F17C2201/056

  Small (<1 m3) · CPC title

• F17C2203/0619

  with two layers · CPC title

• F17C2209/23

  Manufacturing of particular parts or at special locations · CPC title

• F17C2221/012

  Hydrogen · CPC title