The invention discloses an automatic airplane surface heating device, and relates to the technology of airplane surface heating. According to the adopted technical scheme, the automatic airplane surface heating device comprises a tail gas pipeline, a gas valve, a surface heater, a temperature sensor and a valve controller, one end of the tail gas pipeline is used for collecting tail gas of an airplane, the other end of the tail gas pipeline is connected to an air inlet of the surface heater, and the gas valve is arranged inside the tail gas pipeline. The surface heater is used for heating the surface of the airplane. The temperature sensor is used for collecting the temperature of the surface of the airplane and transmitting the collected temperature information to the valve controller. The automatic airplane surface heating device has the advantages that tail gas of the airplane is used for heating the surface of the airplane, and energy consumption and cost are saved.


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    Titel :

    Automatic airplane surface heating device


    Beteiligte:
    DONG GUANGLI (Autor:in) / CHEN CHENG (Autor:in) / HE CHUAN (Autor:in) / CHEN QING (Autor:in) / WU HAIJUN (Autor:in)

    Erscheinungsdatum :

    22.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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