Fuel cell system for supplying aircraft

Details Fuel cell system for supplying aircraft Fuel cell system for supplying aircraft

H - Electricity

01

M

H01M 8/04 (2006.01) H01M 8/00 (2006.01) H01M 8/02 (2006.01) H01M 8/24 (2006.01) H01M 8/08 (2006.01) H01M 8/10 (2006.01)

Patent

CA 2624918

A fuel cell system for aircraft with a passenger cabin comprises a fuel cell. The fuel cell comprises a first inlet connection, a first outlet connection, a cathode side and an anode side, wherein the first inlet connection is formed as the inlet connection of the cathode side and wherein the first outlet connection is formed as the outlet connection of the cathode side. In addition, the fuel cell system is designed in such a way that at the first inlet connection, a gas with a pressure is applied, which corresponds to an air pressure in the passenger machine.

Système de pile à combustible conçu pour un aéronef possédant une cabine pour passagers et consistant en une pile à combustible. Cette dernière comprend un premier raccord d'entrée, un premier raccord de sortie, un côté cathode et un côté anode, ledit premier raccord d'entrée constituant le raccord d'entrée côté cathode et ledit premier raccord de sortie constituant le raccord de sortie côté cathode. Ce système est, de plus, conçu de façon à appliquer un gaz sous pression au niveau du premier raccord d'entrée, ce qui correspond à la pression atmosphérique de la cabine.

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