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    • 2. 发明申请
    • ON BOARD INERT GAS GENERATION SYSTEM
    • WO2012076373A3
    • 2012-06-14
    • PCT/EP2011/071325
    • 2011-11-29
    • EATON AEROSPACE LIMITEDMASSEY, Alan
    • MASSEY, Alan
    • B64D37/32
    • An on board inert gas generation system receives cabin air, or air from another relatively low pressure source, passing a portion thereof through an energy recovery turbine (12) to ambient to extract power which is used to provide all, or part of, the energy required to drive a positive displacement compressor (20) to compress another portion of cabin air to increase the pressure thereof to be suitable for supply to an air separation module (24). The compressed air is then cooled (22) and supplied to the air separation module (24), to generate nitrogen-enriched air for inerting purposes. The cabin air may be used as cooling air for the heating pass of a heat exchanger (22) which extracts heat from the compressed cabin air prior to supply to the air separation module (24). The energy recovery turbine (12) may drive a positive displacement compressor (30) directly, or it may drive a generator (26) whose power is used, optionally in conjunction with power from the aircraft power supply, to drive an electric motor (30) which drives the positive displacement compressor (20).
    • 4. 发明公开
    • ON BOARD INERT GAS GENERATION SYSTEM
    • 在板惰性气体发生系统
    • EP2648977A2
    • 2013-10-16
    • EP11791517.3
    • 2011-11-29
    • Eaton Aerospace Limited
    • MASSEY, Alan
    • B64D37/32
    • B64D37/32A62C3/08A62C99/0018B64D13/08B64D37/24F02C7/25F04C18/16Y02T50/56
    • An on board inert gas generation system receives cabin air, or air from another relatively low pressure source, passing a portion thereof through an energy recovery turbine (12) to ambient to extract power which is used to provide all, or part of, the energy required to drive a positive displacement compressor (20) to compress another portion of cabin air to increase the pressure thereof to be suitable for supply to an air separation module (24). The compressed air is then cooled (22) and supplied to the air separation module (24), to generate nitrogen-enriched air for inerting purposes. The cabin air may be used as cooling air for the heating pass of a heat exchanger (22) which extracts heat from the compressed cabin air prior to supply to the air separation module (24). The energy recovery turbine (12) may drive a positive displacement compressor (30) directly, or it may drive a generator (26) whose power is used, optionally in conjunction with power from the aircraft power supply, to drive an electric motor (30) which drives the positive displacement compressor (20).
    • 机载惰性气体发生系统接收机舱空气或来自另一相对较低压力源的空气,将其一部分通过能量回收涡轮机(12)传送至环境以提取用于提供能量的全部或一部分的能量 需要驱动容积式压缩机(20)以压缩机舱空气的另一部分以增加其压力以适合供应到空气分离模块(24)。 然后将压缩空气冷却(22)并供应到空气分离模块(24),以产生用于惰化目的的富氮空气。 机舱空气可以用作用于热交换器(22)的加热通道的冷却空气,所述热交换器在供应到空气分离模块(24)之前从压缩的机舱空气提取热量。 能量回收涡轮机(12)可以直接驱动容积式压缩机(30),或者可以驱动其动力使用的发电机(26),可选地结合来自飞机电源的动力驱动电动机(30 ),其驱动容积式压缩机(20)。