IP Library Granted Patent US 8,597,844
Granted Patent B2
US 8,597,844 · App. 13/437,176 · Granted Dec 3, 2013

Methods and apparatus for refueling reversible hydrogen-storage systems

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Quick Facts
Patent No.
US 8,597,844
App. No.
13/437,176
Granted
Dec 3, 2013
Kind
B2
Abstract

A method for refilling a hydrogen reservoir comprising a first hydrogen-storing material comprises establishing a fluid connection between the hydrogen reservoir and a cartridge containing a second hydrogen-storing material. The second hydrogen-storing material releases hydrogen at a pressure sufficient to charge the first hydrogen-storing material. Some embodiments involve heating the second hydrogen-storing material and/or allowing heat to flow between the first and second hydrogen-storing materials.

Claims (24)

1. An apparatus comprising:

a portable device comprising

a hydrogen reservoir comprising a first hydrogen-storing material with a charging pressure; and

at least one fuel cell in fluid communication with the hydrogen reservoir; and

a satellite refueling cartridge comprising a second hydrogen-storing material with a plateau pressure that is greater than the charging pressure of the first hydrogen-storing material;

wherein the pressure differential between the charging pressure of the first hydrogen-storing material and the plateau pressure of the second hydrogen-storing material facilitates transfer of the hydrogen from the satellite cartridge into the hydrogen reservoir to charge the first hydrogen-storing material,

wherein the satellite refueling cartridge is in fluid communication with the hydrogen reservoir by way of a detachable fluid coupling

wherein the first and second hydrogen-storing materials are different from one another.

2. The apparatus of claim 1 , wherein the first hydrogen-storing material comprises a metal hydride.

3. The apparatus of claim 1 , wherein the first hydrogen-storing material comprises a material selected from the group consisting of reversible metal hydrides, zeolites, and carbon-based hydrogen-storing materials.

4. The apparatus of claim 1 comprising a continuous thermally-conductive path extending between the first and second hydrogen-storing materials.

5. The apparatus of claim 4 , wherein the continuous thermally-conductive path is configured to allow heat to flow from the first hydrogen-storing material to the second hydrogen-storing material while hydrogen flows from the satellite cartridge into the hydrogen reservoir.

6. The apparatus of claim 1 , wherein when the first and second hydrogen-storing materials are at equal temperatures, the plateau pressure of the second hydrogen-storing material is lower than the charging pressure of the first hydrogen-storing material.

7. The apparatus of claim 1 , comprising a heater disposed to heat the second hydrogen-storing material.

8. The apparatus of claim 7 , wherein the heater is an electrical heater.

9. The apparatus of claim 8 , wherein the electrical heater is configured to be energized when the fluid coupling between the satellite refueling cartridge and the hydrogen reservoir is established.

10. The apparatus of claim 1 , comprising an electrical current source connected to the second hydrogen-storing material, wherein the electrical current source is configured to heat the second hydrogen-storing material by passing an electrical current through the second hydrogen-storing material.

11. The apparatus of claim 1 , wherein the fuel cell is configured to receive hydrogen at a pressure equal to a pressure in the hydrogen reservoir.

12. The apparatus of claim 1 , comprising a pressure regulator disposed in a fluid path between the hydrogen reservoir and the fuel cell, the pressure regulator configured to provide hydrogen to the fuel cell at a pressure that is lower than a pressure within the hydrogen reservoir.

13. The apparatus of claim 1 , wherein the portable device comprises a fuel cell layer in fluid communication with the hydrogen reservoir, wherein the fuel cell layer includes the at least one fuel cell.

14. The apparatus of claim 1 , further comprising a closure mechanism that when opened is configured to allow the fluid communication of the satellite refueling cartridge with the hydrogen reservoir.

15. The apparatus of claim 1 , wherein the satellite refueling cartridge is in fluid communication with the hydrogen reservoir via a detachable fluid coupling.

16. The apparatus of claim 15 , wherein the detachable fluid coupling comprises a magnetic coupling.

17. The apparatus of claim 15 , wherein the detachable fluid coupling is a coupling selected from the group comprising threaded couplings, magnetic couplings, bayonet couplings, and adhesive couplings.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 6, 2015
From: SOCIÉTÉ BIC
To: INTELLIGENT ENERGY LIMITED
Reel/Frame 036303/0915 →