AIRCRAFT ENVIRONMENTAL CONDITIONING SYSTEM AND METHOD
    22.
    发明申请
    AIRCRAFT ENVIRONMENTAL CONDITIONING SYSTEM AND METHOD 审中-公开
    飞机环境调节系统及方法

    公开(公告)号:US20150314878A1

    公开(公告)日:2015-11-05

    申请号:US14616129

    申请日:2015-02-06

    Abstract: An aircraft environmental conditioning system is disclosed having an air cycle machine for conditioning an airflow comprising hot compressed air by reducing its temperature and pressure. The air cycle machine is disposed in a housing in an unpressurized area of the aircraft, and produces conditioned pressurized air for delivery to a pressurized area of the aircraft. The system also includes a vibration sensor disposed within the housing, and a controller in communication with the vibration sensor that is configured to respond to vibration detected by the vibration sensor.

    Abstract translation: 公开了一种具有用于通过降低其温度和压力来调节包含热压缩空气的气流的空气循环机的飞机环境调节系统。 空气循环机设置在飞行器的非加压区域中的壳体中,并且产生用于输送到飞行器的加压区域的经调节的加压空气。 该系统还包括设置在壳体内的振动传感器,以及与振动传感器通信的控制器,该控制器被配置为响应由振动传感器检测到的振动。

    COOLED AIR SOURCE FOR CATALYTIC INERTING
    25.
    发明申请

    公开(公告)号:US20190283898A1

    公开(公告)日:2019-09-19

    申请号:US15924525

    申请日:2018-03-19

    Abstract: An aircraft inert gas generating system includes a fuel source configured to supply fuel, a stream of reaction air having a first temperature, an air-fuel mixing unit configured to receive an amount of the fuel and an amount of the reaction air stream to create an air-fuel mixture, and a catalytic oxidation unit configured to receive and react the air-fuel mixture. The stream of reaction air includes an amount of mixing air from a mixing air source, and the mixing air source includes a primary heat exchanger of an aircraft ram circuit and a cooling air extraction element proximate the heat exchanger. The mixing air can alternatively include cool air from a heat sink air source.

    FUEL TANK INERTING SYSTEMS FOR AIRCRAFT
    29.
    发明申请

    公开(公告)号:US20170313435A1

    公开(公告)日:2017-11-02

    申请号:US15499067

    申请日:2017-04-27

    CPC classification number: B64D37/32 B01D53/22 B01D2053/224 B64D13/06 B64D13/08

    Abstract: Aircraft air separation systems having a compressed air source arranged to supply compressed air, an air separation module arranged to receive air from the compressed air source, the air separation module arranged to separate air into nitrogen enriched air and oxygen enriched air, wherein the nitrogen enriched air is supplied to a fuel tank of the aircraft, and a source of mixing air arranged to fluidly supply the mixing air at a location between the compressed air source and the air separation module such that the mixing air is selectively mixed with the compressed air to generate treated air that is supplied to the air separation module.

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