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    AIRCRAFT SYSTEMS AND METHODS WITH GREEN FUEL TANKS
    3.
    发明申请
    AIRCRAFT SYSTEMS AND METHODS WITH GREEN FUEL TANKS 审中-公开
    具有绿色燃油箱的飞机系统和方法

    公开(公告)号：US20150266589A1

    公开(公告)日：2015-09-24

    申请号：US14223428

    申请日：2014-03-24

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Eric Blumer ,  Mukund Acharya ,  Audie Mak ,  Mario Scaini ,  Bijan F. Hagh

    IPC: B64D37/00 ,  H01M8/06 ,  B64D37/34 ,  B64D41/00 ,  B64D37/02 ,  B64D37/30

    CPC classification number: B64D37/00 ,  B64D37/02 ,  B64D37/30 ,  B64D37/34 ,  B64D41/00 ,  F02C9/40 ,  H01M8/0625 ,  H01M2250/20 ,  Y02T50/44 ,  Y02T50/671 ,  Y02T50/678 ,  Y02T90/32

    Abstract: An aircraft system includes a main fuel tank configured to house primary fuel and a green fuel tank configured to house green fuel. The mixing apparatus is configured to mix the primary fuel and the green fuel to result in a predetermined ratio of mixed fuel. A controller selectively commands a first amount of primary fuel and a second amount of green fuel to result in the predetermined ratio of mixed fuel. The main aircraft engine is configured to operate, in a first main engine mode, with the primary fuel from the main fuel tank and to operate, in a second main engine mode, with the mixed fuel from the mixing apparatus based on commands from the controller. The auxiliary power source is configured to operate with at least a portion of the green fuel from the green fuel tank based on commands from the controller.

    Abstract translation: 飞机系统包括：主燃料箱，其构造成容纳一次燃料;以及绿色燃料箱，其构造成容纳绿色燃料。 混合装置被配置为混合初级燃料和绿色燃料以产生混合燃料的预定比例。 控制器选择性地命令第一量的初级燃料和第二量的绿色燃料导致混合燃料的预定比例。 主飞机发动机被构造成以第一主发动机模式与来自主燃料箱的主燃料一起操作，并且在第二主发动机模式下，基于来自控制器的命令从混合装置操作混合燃料 。 辅助动力源被配置为基于来自控制器的命令与来自绿色燃料箱的绿色燃料的至少一部分一起操作。

    AIRCRAFT SYSTEMS AND METHODS WITH INTEGRATED TANK INERTING AND POWER GENERATION
    5.
    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

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Bijan F. Hagh ,  Daguang Zheng ,  Russell W. Johnson ,  Mukund Acharya ,  Mario Scaini

    IPC: B64D37/32 ,  A62C3/06 ,  A62C3/08

    CPC classification number: B64D37/32 ,  A62C3/065 ,  A62C3/08 ,  B64D41/00 ,  B64D2041/005 ,  F02C3/04 ,  F02C6/00 ,  F02C7/22 ,  F05D2220/50 ,  F05D2220/76 ,  F05D2240/35 ,  H01M8/04014 ,  H01M8/04111 ,  H01M8/0618 ,  H01M2250/20 ,  Y02E60/50 ,  Y02T90/32 ,  Y02T90/36

    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。

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