Liquid hydrogen storage system as thermal battery
A cooling system and cooling method for a fuel cell onboard a vehicle, wherein the fuel cell includes a gasifier configured to expand liquid hydrogen to gaseous hydrogen for feed to the fuel cell, the cooling system including a coolant system sized for less than peak power operation of the vehicle; and an auxiliary coolant system configured to provide supplemental cooling to the fuel cell, wherein the supplemental coolant system is configured to by-pass coolant to the gasifier and employ heat of gasification of the liquid hydrogen to provide supplemental cooling for the fuel cell during peak vehicle operation.
1. A cooling system for a fuel cell onboard a vehicle, wherein the fuel cell includes a gasifier configured to expand liquid hydrogen to gaseous hydrogen for feed to the fuel cell, the cooling system comprising:
a coolant system sized below that required for peak power operation of the vehicle; and
an auxiliary coolant system configured to provide supplemental cooling to the fuel cell, wherein the supplemental coolant system is configured to by-pass coolant to the gasifier and employ heat of gasification of the liquid hydrogen to provide supplemental cooling for the fuel cell during peak vehicle operation.
2. The cooling system of claim 1 , wherein the auxiliary coolant system includes an accumulator tank for accumulating excess gaseous hydrogen created by the auxiliary cooling system.
3. The cooling system of claim 2 , wherein the accumulator tank comprises a variable volume tank.
4. The cooling system of claim 3 , wherein the variable volume tank comprises a balloon or bellows tank.
5. The cooling system of claim 1 , wherein the auxiliary coolant system is configured to vent at least a portion of the hydrogen after gasification.
6. The cooling system of claim 1 , wherein the coolant system sized below that required for peak power operation of the vehicle comprises a phase-change coolant system.
7. The cooling system of claim 1 , further including a controller configured to control operation of the coolant system sized below that required for peak power operation of the vehicle and operation of the auxiliary coolant system.
8. The cooling system of claim 7 , wherein the controller is programmed to control one or more of {operation of valves and pumps of the cooling system}, {flow of coolant and hydrogen depending on cooling demands}, and {liquid hydrogen level, temperature and pressure of the liquid hydrogen passed to the gasifier, depending on one or more of fuel cell power requirements, fuel cell temperature, fuel cell maximum design operating temperature and Outside Air Temperature (OAT)}.
9. The cooling system of claim 1 , wherein the vehicle comprises a fuel cell powered aircraft.
10. A method for cooling a fuel cell aboard a vehicle, wherein the fuel cell includes a cooling system and a gasifier configured to expand liquid hydrogen to gaseous hydrogen for feed to the fuel cell, comprising the steps of:
providing a coolant system sized below that required for peak power operation of the vehicle and an auxiliary coolant system configured to provide supplemental cooling to the fuel cell, wherein the auxiliary coolant system is configured to by-pass coolant to the gasifier, and
activating the auxiliary coolant system during peak vehicle operation, employing heat of gasification of the liquid hydrogen to provide supplemental cooling for the fuel cell.
11. The method of claim 10 , wherein the auxiliary coolant system includes an accumulator tank for accumulating excess gaseous hydrogen created by the auxiliary coolant system.
12. The method of claim 11 , wherein the accumulator tank comprises a variable volume tank.
13. The method of claim 12 , wherein the variable volume tank comprises a balloon or bellows tank.
14. The method of claim 10 , wherein the auxiliary coolant system is configured to vent at least a portion of the hydrogen after gasification, and including the step of venting a portion of the hydrogen.
15. The method of claim 10 , wherein the coolant system sized below that required for peak power operation of the vehicle comprises a phase-change coolant system.
16. The method of claim 10 , wherein the cooling system further includes a controller configured to control operation of the coolant system sized below that required for peak power operation of the vehicle and the auxiliary coolant system, and including the step of controlling operation of the cooling system based on vehicle operating conditions and environmental conditions.
17. The method of claim 16 , wherein the controller is programmed to control operation of valves and pumps of the cooling system and flow of coolant depending on cooling demands, and to control liquid hydrogen level, temperature and pressure of the liquid hydrogen passed to the gasifier, depending on one or more of fuel cell power requirements, fuel cell temperature, fuel cell maximum design operating temperature and Outside Air Temperature (OAT).
18. The method of claim 10 , wherein the vehicle comprises a fuel cell powered aircraft.