The invention relates to a vertical take-off and landing (VTOL) efficient and high-speed aircraft. A combined type longitudinal variable-wing reverse-speed rotor aircraft is characterized in that a main lift rotor set 5 is longitudinally arranged on the upper portion of an aircraft body 1, two pairs of convertible paddles 9 are arranged on the main lift rotor set 5, a fixed wing 2 is arranged in the middle of the aircraft body 1, a forward flying power system 4 is arranged on the aircraft body 1, and ailerons 8 are arranged on the fixed wing 2; a horizontal tail 3, a vertical tail 6 and an undercarriage 7 are arranged on the aircraft body 1. Rotor-wing conversion enables the combined type longitudinal variable-wing reverse-speed rotor aircraft to truly become a high-speed helicopter capable of vertically taking off, landing and hovering, and the combined type longitudinal variable-wing reverse-speed rotor aircraft has great significance in national economy and national defense construction.

    本发明涉及一种垂直起降(VTOL)高效、高速飞行器。复合式纵列变翼逆速旋翼飞行器,其特征在于机体1上部纵列布置主升力旋翼组5,主升力旋翼组5上布置有两副可转换桨叶9,机体1中部布置有固定机翼2,机体1上布置有前飞动力系统4,固定机翼2上布置有副翼8,机体1上布置有水平尾翼3、垂直尾翼6、起落架7。旋翼—机翼转换使复合式纵列变翼逆速旋翼飞行器真正成为一款可垂直起降、悬停的高速直升飞机,在国民经济及国防建设中具有重大意义。


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    Title :

    Combined type longitudinal variable-wing reverse-speed rotor aircraft


    Additional title:

    复合式纵列变翼逆速旋翼飞行器


    Contributors:
    FAN LEI (author)

    Publication date :

    2020-12-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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