The invention provides a composite high-speed helicopter, which relates to the technical field of helicopters and comprises a helicopter body, fixed wings, rotor wings and tail rotors, fixed wings are only arranged on one side of the fuselage, rotors are arranged at the top of the fuselage, and a tail rotor is arranged at the tail of the fuselage; a movable flap is arranged on the rear edge of the fixed wing. According to the scheme provided by the invention, shock waves during high-speed forward flight can be delayed, the problem that a conventional helicopter cannot stably fly at a high speed is solved, and the attitude is stable in the forward flight process.

    本发明提供一种复合式高速直升机,涉及直升机技术领域,包括:机身、固定翼、旋翼、尾桨;仅在机身的一侧配置固定翼,旋翼配置于机身顶部,机身尾部配置有尾桨;固定翼后缘配置有可动襟翼。本发明提供的方案能够推迟大速度前飞时激波的出现,解决了常规直升机不能稳定高速飞行的难题,且前飞过程中姿态稳定。


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    Titel :

    Combined type high-speed helicopter


    Weitere Titelangaben:

    一种复合式高速直升机


    Beteiligte:
    KONG WEIHONG (Autor:in) / LIANG XIAOCHEN (Autor:in) / CHAO ZHENGXIANG (Autor:in) / LI PAN (Autor:in)

    Erscheinungsdatum :

    2023-12-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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