AIRCRAFT VAPOUR TRAIL CONTROL SYSTEM
    1.
    发明申请
    AIRCRAFT VAPOUR TRAIL CONTROL SYSTEM 有权
    飞机蒸汽拖车控制系统

    公开(公告)号:US20150285158A1

    公开(公告)日:2015-10-08

    申请号:US14644799

    申请日:2015-03-11

    Abstract: The invention concerns an aircraft propulsion control system in which a gas turbine engine has an actuable flow opening for control of flow to or from a portion of the engine. One or more sensor is arranged to sense a condition indicative of vapour trail formation by the exhaust flow from the engine. A controller is arranged to control actuation of the flow opening so as to reduce the efficiency of the engine upon sensing of said condition by the one or more sensor. In one example, the flow opening is a variable area fan nozzle.

    Abstract translation: 本发明涉及一种飞机推进控制系统,其中燃气涡轮发动机具有用于控制流向或来自发动机的一部分的流动的可启动流动开口。 一个或多个传感器被布置成通过来自发动机的排气流感测指示蒸气轨道形成的状况。 控制器被布置成控制流动开口的致动,以便在通过一个或多个传感器检测到所述状态时降低发动机的效率。 在一个示例中,流动开口是可变区域风扇喷嘴。

    CARBON DIOXIDE CAPTURE
    3.
    发明公开

    公开(公告)号:US20230347276A1

    公开(公告)日:2023-11-02

    申请号:US18025953

    申请日:2021-08-23

    Abstract: A system for capture of atmospheric carbon dioxide. The system includes a carbon dioxide capture device having a capture medium operable to capture atmospheric carbon dioxide under a first set of thermodynamic conditions, and to release carbon dioxide under a second set of thermodynamic conditions different to the first set of thermodynamic conditions. The first set of thermodynamic conditions includes a first temperature range and the second set of thermodynamic conditions includes a second temperature range. A heat engine is configured receive a working fluid at an inlet temperature and arranged to discharge at least a portion of the working fluid at a discharge temperature in the second temperature range or higher, and a heat transfer arrangement is configured to convey heat from discharged working fluid to the capture medium to release carbon dioxide therefrom.

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