IP Library › Granted Patent US 10,934,165
Granted Patent B2
US 10,934,165 · App. 15/744,892 · Granted Mar 2, 2021

Solid hydrogen storage system

Inventors: Colin John Halsey (Tewkesbury, GB); Alexander James Rainbow (Swindon, GB)
Assignee: GE AVIATION SYSTEMS LIMITED
C01B3/065C01B3/001C01B3/0005C01B3/04C01B3/06H01M8/065H01M8/0643B64D2041/005H01M2250/20Y02E60/32Y02E60/36Y02T90/40
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,934,165
App. No.
15/744,892
Granted
Mar 2, 2021
Kind
B2
Abstract

A hydrogen storage system includes a pressure-sealed sleeve defining an interior and having an outlet, a shaft extending through the interior of the sleeve, a set of porous chambers arranged axially along and concentric to the shaft, and a hydrogen storage, wherein at least some hydrogen gas is supplied to the outlet.

Claims (22)

1. A solid hydrogen storage system, comprising:

a pressure-sealed sleeve defining an interior and having an outlet;

a shaft extending through the interior of the sleeve;

a set of circularly shaped porous chambers arranged axially along and concentric to the shaft and wherein each of the set of circularly shaped porous chambers includes a porous basket and a porous lid; and

a hydrogen storage solid held by the set of circularly shaped porous chambers wherein a chemical reaction liberates hydrogen gas from the hydrogen storage solid, through the set of circularly shaped porous chambers, and the hydrogen gas is supplied to the outlet.

2. The storage system of claim 1 , wherein the shaft is a hollow shaft fluidly coupled with a water reservoir and further includes a set of ports configured to deliver water received from the water reservoir to the interior of the pressure-sealed sleeve.

3. The storage system of claim 2 , wherein the set of circularly shaped porous chambers are at least one of water-permeable or steam-permeable.

4. The storage system of claim 1 , wherein the hydrogen storage solid is at least one of a metal hydride, lithium hydride, or lithium hydroxide.

5. The storage system of claim 1 , wherein the shaft further comprises a set of shaft segments configured to axially couple with adjacent shaft segments, and a shaft segment includes the porous basket and the porous lid.

6. The storage system of claim 5 , wherein the set of circularly shaped porous chambers comprises the porous lid of a first shaft segment and the porous basket of a second adjacent shaft segment.

7. The storage system of claim 1 , wherein the hydrogen storage solid is a powder.

8. The storage system of claim 1 , wherein the chemical reaction is non-reversible.

9. The storage system of claim 1 , wherein the outlet is fluidly coupled with a fuel cell.

10. The storage system of claim 1 , wherein the pressure-sealed sleeve is configured for exposure to pressure up to 15 bar.

11. The storage system of claim 1 , wherein the set of circularly shaped porous chambers are configured to deform in response to an expansion of the hydrogen storage solid due to the chemical reaction.

12. A method of releasing hydrogen gas from the solid hydrogen storage system of claim 1 , the method comprising:

receiving, by a control module, a demand signal indicative of a demand for hydrogen gas; and

in response to receiving the demand signal, controlling, by the control module, the initiation of a chemical reaction in at least a portion of the pressure-sealed sleeve having the set of circularly shaped porous chambers holding the hydrogen storage solid, by selectively supplying at least one of water or heat to the at least a portion of pressure-sealed sleeves, wherein the chemical reaction liberates hydrogen gas from the hydrogen storage solid, and wherein the liberated hydrogen gas is proportional to the demand for hydrogen gas.

13. The method of claim 12 , wherein the controlling further includes staggering the initiating of the chemical reaction in the at least a portion of pressure-sealed sleeves to maintain the pressure of the hydrogen gas between 6 bar and 15 bar.

14. The method of claim 12 , further comprising delivering the liberated hydrogen gas to a fuel cell and generating electricity in the fuel cell from the liberated hydrogen gas.

15. The method of claim 12 , wherein the receiving the demand signal is further indicative of an emergency power demand in an aircraft.

16. The method of claim 12 , further comprising replacing the at least a portion of pressure-sealed sleeves after the chemical reaction has ceased.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 15, 2018
From: HALSEY, COLIN JOHN; RAINBOW, ALEXANDER JAMES
To: GE AVIATION SYSTEMS LIMITED
Reel/Frame 044620/0014 →
Continuity (1)
Related Publication 20180208463A1 · Jul 26, 2018