The invention discloses a compound type rotor wing lift device, which belongs to the technical field of aircrafts. The compound type rotor wing lift device comprises a spindle, a rotor wing head, a power device as well as two, three or four identical composite wings which are uniformly distributed around the rotor wing head, wherein each composite wing comprises a foil and two, three or four propellers with identical parameters; the leading edge of each foil is horizontally arranged; the root of each foil is connected with the rotor wing head; the leading edge of each foil is higher than the trailing edge of the foil; all the propellers are arranged below the foils in a linearly horizontal or forward inclined way; the propellers of all the composite wings are driven by one engine, or each propeller is separately equipped with one engine; since the propellers are arranged below the foils, and air current above the foils is led to the rear-lower part when the propellers rotate, air current separation of the upper surfaces of the foils can be put off, and the efficiency and the stability are favorably improved; in addition, attack angles of the foils can be greater, so that that a lifting force generated in unit area of the foils is improved; the device is arranged on an aircraft as the lift device.


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    Titel :

    Compound type rotor wing lift device


    Beteiligte:
    WANG ZHICHENG (Autor:in)

    Erscheinungsdatum :

    06.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge