Thermally activated safety valve for pressure vessels
AssigneeGM Global Technology Operations LLC
InventorUwe Suess
Life of this patent
Estimating the term…
Abstract
A pressure vessel is provided having an outer support layer having an inner surface; a composite wrap disposed adjacent to the inner surface; and a liner disposed adjacent to the fiber composite wrap. Further provided is an adapter disposed at a first end of the pressure vessel and configured for charging a cavity formed by the pressure vessel with a compressed fuel, wherein the adapter includes a first pressure relief device; and a second pressure relief device disposed at a second end of the pressure vessel. The second pressure relief device defines a passage through the outer support layer and the composite wrap and has a chamber and a diaphragm disposed between the chamber and the cavity. Also described are a fuel cell propulsion system and a vehicle including the provided pressure vessel.
Claims20
A pressure vessel comprising:
- an outer support layer having an inner surface;
- a liner disposed adjacent to the inner surface of the outer support layer, an inner surface of the liner defining a closed cavity within the pressure vessel and
- a first pressure relief device disposed in the outer support layer, the first pressure relief device having:
- a main body with a chamber enveloping a chamber material, the chamber material filling the chamber, and
- a diaphragm abutting the liner and disposed between the chamber and the cavity, the chamber material abutting the diaphragm and supporting the diaphragm against a pressure of the cavity,
- wherein the diaphragm is adapted to rupture upon activation of the first pressure relief device and facilitate an evacuation of the chamber material and a compressed fuel from the cavity through the pressure relief device.
A pressure vessel comprising:
- an outer support layer having an inner surface;
- a composite wrap disposed adjacent to the inner surface;
- a polymeric liner disposed adjacent to the composite wrap, an inner surface of the liner defining a closed cavity within the pressure vessel;
- an adapter disposed at a first end of the pressure vessel and configured for charging the cavity with a compressed fuel, wherein the adapter includes a first pressure relief device;
- a second pressure relief device disposed in the outer support layer, the second pressure relief device having:
- a main body with a chamber enveloping a chamber material, the chamber material filling the chamber, and
- a diaphragm abutting the liner and disposed between the chamber and the cavity, the chamber material abutting the diaphragm and supporting the diaphragm against a pressure of the cavity,
- wherein the diaphragm is adapted to rupture upon activation of the second pressure relief device and facilitate an evacuation of the chamber material and a compressed fuel from the cavity through the second pressure relief device.
A fuel cell propulsion system comprising:
- a fuel cell system having a fuel cell stack including a plurality of fuel cells, the fuel cell stack being configured to receive a compressed fuel from a pressure vessel;
- the pressure vessel comprising:
- an outer support layer having an inner surface;
- a composite wrap disposed adjacent to the inner surface;
- a liner disposed adjacent to the fiber composite wrap, an inner surface of the liner defining a closed cavity within the pressure vessel;
- an adapter disposed at a first end of the pressure vessel and configured for filling the cavity formed by the liner with the compressed fuel, wherein the adaptor includes a first pressure relief device;
- and a second pressure relief device disposed at a second end of the pressure vessel and forming a passage through the outer support layer and the composite wrap,
- the second pressure relief device having:
- a main body with a chamber enveloping a chamber material, the chamber material filling the chamber, and
- a diaphragm abutting the liner and disposed between the chamber and the cavity, the chamber material abutting the diaphragm and supporting the diaphragm against a pressure of the cavity,
- wherein the diaphragm is adapted to rupture upon activation of the pressure relief device and facilitate an evacuation of the chamber material and a compressed fuel from the cavity through the pressure relief device.
Dependencies are inferred from the claim text.