The invention provides a tiltrotor mixed multi-state aircraft. The aircraft comprises a fuselage which contains two parallelly and symmetrically arranged fixed wings and a middle support frame. There are four rotor wings on the two fixed wings. According to the aircraft, advantages of a multi-rotor aircraft and a fixed-wing aircraft are integrated, and multi-rotor wings are mounted on the multiple fixed wings. In all parts, propellers and a rotating shaft of a motor can rotate normally, but relative positions of the other parts are not changed. Especially the mounting positions of the fuselage, the motor and the propellers are relatively fixed. The aircraft has three flight states: a vertical take-off and landing or spot hover state, a cruising flight state and a transition state.


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    Titel :

    Tiltrotor mixed multi-state aircraft


    Beteiligte:
    WANG YINGCHUN (Autor:in) / WANG HONGYU (Autor:in) / LIU LING (Autor:in) / CHEN SHIMING (Autor:in) / WANG MINGCAI (Autor:in) / DIAO QIZHUO (Autor:in)

    Erscheinungsdatum :

    28.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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