The invention discloses a flying vehicle. The flying vehicle comprises a first main vehicle body (1), a second main vehicle body (2), a connecting wing unit (3), control surfaces and propelling systems, wherein the connecting wing unit (3) connects the first main vehicle body (1) with the second main vehicle body (2); the control surfaces are arranged on the first main vehicle body (1) and the second main vehicle body (2) respectively; the propelling systems are arranged on the first main vehicle body (1) and the second main vehicle body (2) respectively; the control surfaces are used for controlling flight attitudes of the flight vehicle; the propelling systems are used for providing power for the flight vehicle. The flight vehicle has the two main vehicle bodies, compared with a bladder type double-body flight vehicle, the layout formed by the two independent main vehicle bodies and the connecting wing unit which connects the two main vehicle bodies is adopted, larger lift force can be provided, the amount of fuel which can be carried is increased, the flight vehicle can be further lifted by utilizing the space below the connecting wing unit, more transportation modes can be selected, and the possibility of conducting task development such as continuous monitoring is provided.


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    Titel :

    Flight vehicle


    Beteiligte:
    CHAI JIANZHONG (Autor:in) / GAO XU (Autor:in)

    Erscheinungsdatum :

    2015-11-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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





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