The invention discloses a glove vane aircraft. The glove vane aircraft comprises a first glove vane (2) and a second glove vane (3) which are symmetrical to each other about an aircraft body (1). Glove vane rollers (4) are arranged on the first glove vane (2) and the second glove vane (3). In the aircraft running state, roller bodies (41) in the glove vane rollers (4) bear air flow opposite to the running direction of the aircraft. The glove vane aircraft is characterized in that the glove vane aircraft further comprises a high lift device (5) which is arranged on the air inlet sides of the glove vane rollers (4) and used for providing a power source for the glove vane rollers (4), and therefore the glove vane rollers (4) can obtain extra power. Due to the adoption of the structure, for the same glove vane aircraft, the running distance of the glove vane aircraft can be greatly reduced, and in other words, the glove vane roller lift force conversion efficiency of the glove vane aircraft is improved.


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    Titel :

    Glove vane aircraft


    Beteiligte:
    LI YUELI (Autor:in) / CHEN TAO (Autor:in) / LI JUNFU (Autor:in) / TAN RONGRONG (Autor:in)

    Erscheinungsdatum :

    21.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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