The invention relates to the field of aviation, in particular to a petrol-electric hybrid power airship. The petrol-electric hybrid power airship comprises an airship body (1) and a power device (2), and the power device (2) is arranged below the airship body (1). The petrol-electric hybrid power airship is characterized in that the power device (2) is a petrol-electric hybrid power device and comprises three propellers (21, 22, 23), wherein two of the propellers (21, 22) are electric propellers, and one propeller (23) is liquid fuel power propeller. According to the petrol-electric hybrid power airship, the liquid fuel power propeller and the electric propellers are organically combined, so that control response of the airship in the aviation process can be rapidly achieved, and the flight posture is rapidly adjusted so that different aviation requirements can be met.


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    Titel :

    Petrol-electric hybrid power airship


    Beteiligte:
    WU HONGHUI (Autor:in) / SU CHENGYUE (Autor:in) / XIAO JIADONG (Autor:in) / ZHU LIUZHOU (Autor:in) / HUANG RIHENG (Autor:in) / XU SHUQI (Autor:in) / LIN ZHICONG (Autor:in) / SHI ZHENHUA (Autor:in)

    Erscheinungsdatum :

    2016-02-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft



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