본 개시는, 연료 전지(110), 연료 탱크(130), 상기 연료 전지(110)의 연료 주입구(116)와 상기 연료 탱크(130)를 유체 연통 가능하게 연결하는 연료 분배 파이프(135), 상기 연료 분배 파이프(135)의 적어도 일부를 둘러싸는 슈라우드(137), 질소가 풍부한 공기(NEA) 및 산소가 풍부한 공기(OEA)를 생성하도록 구성된 불활성화 시스템(inerting system)(120) 및 상기 질소가 풍부한 공기를 상기 슈라우드(137)로 전달하는 NEA 파이프(124)를 포함하는, 연료 전지 시스템(100)에 관한 것이다.

    The present disclosure relates to a fuel cell system (100) comprising a fuel cell (110), a fuel tank (130), a fuel distribution pipe (135) fluidly connecting the fuel tank (130) with a fuel inlet (116) of the fuel cell (110), a shroud (137) surrounding at least a portion of the fuel distribution pipe (135), an inerting system (120) configured to generate nitrogen enriched air, NEA, and oxygen enriched air, OEA, and an NEA pipe (124) conducting the nitrogen enriched air into the shroud (137).


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    Title :

    FUEL CELL SYSTEM AND AIRCRAFT HAVING AN INERTING SYSTEM


    Additional title:

    불활성화 시스템을 구비한 연료 전지 시스템 및 항공기


    Contributors:
    BECKS RALF (author)

    Publication date :

    2024-11-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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