AIRCRAFT SYSTEMS AND METHODS WITH INTEGRATED TANK INERTING AND POWER GENERATION
    21.
    发明申请
    AIRCRAFT SYSTEMS AND METHODS WITH INTEGRATED TANK INERTING AND POWER GENERATION 有权
    具有集成油罐加油和发电的飞机系统和方法

    公开(公告)号:US20150353201A1

    公开(公告)日:2015-12-10

    申请号:US14227689

    申请日:2014-03-27

    Abstract: A system is provided for inerting a fuel tank of an aircraft. The system includes a first compressor fluidly coupled to the fuel tank for removing an air and fuel vapor mixture from an ullage of the fuel tank. The system further includes a fuel processor fluidly coupled to the first compressor and configured to receive the air and fuel vapor mixture and to generate hydrogen from the air and fuel vapor mixture. The system further includes a fuel cell fluidly coupled to the fuel processor and configured to receive the hydrogen as anode fuel to produce electricity. The system further includes a combustor fluidly coupled to the fuel cell and configured to combust the exhaust product to produce combustion gas, and a first heat exchanger fluidly coupled to the combustor and configured to cool the combustion gas into inerting gas for the fuel tank.

    Abstract translation: 提供一种用于使发动机的燃料箱无效的系统。 该系统包括流体地联接到燃料箱的第一压缩机,用于从燃料箱的空缺中去除空气和燃料蒸汽混合物。 该系统还包括流体耦合到第一压缩机并被配置为接收空气和燃料蒸汽混合物并从空气和燃料蒸气混合物产生氢气的燃料处理器。 该系统还包括流体耦合到燃料处理器并被配置为接收氢作为阳极燃料以产生电力的燃料电池。 该系统还包括流体地联接到燃料电池并且被配置为燃烧排气产品以产生燃烧气体的燃烧器,以及流体地联接到燃烧器并且被配置为将燃烧气体冷却成用于燃料箱的惰化气体的第一热交换器。

Patent Agency Ranking