|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||429/439; 429/400; 429/456|
|우선권정보||DE-10 2006 034 816 (2006-07-27)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 3 인용 특허 : 2|
A cooling system for cooling a fuel-cell system on board an aircraft, in one example, includes a hydrogen accumulator, a connecting device coupling the hydrogen accumulator, with an external cooling system for dissipating heat arising upon charging of the hydrogen accumulator. The hydrogen accumulator cools down upon removal of hydrogen, because of which cooling of a condenser occurs. The cooling system need not utilize a secondary cooling loop for condenser cooling.
1. A cooling system for cooling a fuel-cell system on board an aircraft, the fuel cell system comprising: a fuel cell; anda water condenser;wherein the cooling system comprises: a hydride accumulator integrated in the fuel cell; anda connection device coupling an external cooling system with the hydride accumulator and a coupler coupling the hydride accumulator to an external source hydrogen for charging the hydride accumulator with hydrogen;wherein the hydride accumulator is arranged such that the fuel-cell is cooled only during discharge of hydrogen fr...