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。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Combined type longitudinal variable-wing reverse-speed rotor aircraft


    Weitere Titelangaben:

    复合式纵列变翼逆速旋翼飞行器


    Beteiligte:
    FAN LEI (Autor:in)

    Erscheinungsdatum :

    2020-12-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



    Composite tilting wing tandem variable-wing reverse-speed rotor aircraft

    FAN LEI | Europäisches Patentamt | 2020

    Freier Zugriff

    Composite tilting power tandem variable-wing reverse-speed rotor aircraft

    FAN LEI | Europäisches Patentamt | 2020

    Freier Zugriff

    Combined type rotor wing transmission system and combined type rotor wing aircraft

    QI ZHIGANG / ZHANG SHILONG / ZHANG JIECHAO et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Combined type single-row rotor wing tilting aircraft

    GAO YUJIAN | Europäisches Patentamt | 2022

    Freier Zugriff

    Variable-pitch variable-speed rotor wing

    ZHANG DEMING / FEI CHENGWEI / LI HAODONG et al. | Europäisches Patentamt | 2024

    Freier Zugriff