The invention discloses an intermediate shaft tilt rotor aircraft which comprises a main rotor (1), a main rotor shaft (2), a reversing connecting mechanism (3), an engine (4), a fixed wing (5), an aircraft body (6) and a tail rotor (7), the main rotor shaft (2) is arranged at the gravity center of the aircraft body (6), the main rotor (1) is arranged at the top end of the main rotor shaft (2), the main rotor shaft (2) is attached to and fixedly connected with the transverse center line of the fixed wing (5), and the transverse center line of the fixed wing (5) corresponds to the gravity center of the aircraft body (6). The reversing connecting mechanism (3) is arranged between the main rotor shaft (2) and the aircraft body (6), the reversing connecting mechanism (3) is movably connected with the aircraft body (6) and the main rotor shaft (2), and the engine (4) is arranged in the middle of the fixed wing (5). The unmanned aerial vehicle is ingenious in design, simple in structure, safe in function and efficient in maneuvering.

    本发明公开了一种中间轴倾转旋翼飞机,包括主旋翼(1)、主旋翼轴(2)、换向连接机构(3)、发动机(4)、固定翼(5)、机体(6)、尾桨(7),机体(6)上重心处设置主旋翼轴(2),主旋翼轴(2)顶端设置主旋翼(1),主旋翼轴(2)与固定翼(5)的横向中线贴合并固定连接,固定翼(5)横向中线与机体(6)重心对应,换向连接机构(3)设置在主旋翼轴(2)和机体(6)之间,换向连接机构(3)与机体(6)活动连接,换向连接机构(3)与主旋翼轴(2)活动连接,发动机(4)设置在固定翼(5)中部,本发明设计巧妙,结构简单,功能安全,机动高效。


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    Titel :

    Intermediate shaft tilt rotor aircraft


    Weitere Titelangaben:

    一种中间轴倾转旋翼飞机


    Beteiligte:
    YANG JINGKE (Autor:in)

    Erscheinungsdatum :

    2022-04-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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