The invention relates to the field of vertical take-off and landing aircrafts, in particular to a gravity telescopic tail base and a vertical take-off and landing tilting flat flight aircraft, which comprise an aircraft body, a coaxial reverse propeller power device is arranged at the front end of the aircraft body, a left wing and a right wing are symmetrically arranged on two sides of the aircraft body, and the gravity telescopic tail base is arranged at the central axis position of the aircraft body. The gravity telescopic tail base can do telescopic motion through gravity during vertical take-off and landing, the gravity telescopic tail base moves backwards by a certain distance to change the shape, the shape of the aircraft with the changed shape is close to that of a conventional fixed-wing aircraft, and the performance of the aircraft is close to that of the conventional fixed-wing aircraft.

    本发明重力可伸缩机尾座及垂直起降倾转平飞飞行器为垂直起降飞行器领域,包括机体,所述机体前端设有一套所述共轴反桨动力装置、两侧对称设有左翼和右翼,所述机体中轴位置设有重力可伸缩机尾座,所述重力可伸缩机尾座垂直起降时利用重力可进行伸缩运动,所述重力可伸缩机尾座向后移动一定的距离改变形状,改变形状后的所述飞行器的形状接近常规固定翼飞机的形状,性能也接近常规固定翼飞机的性能。


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    Titel :

    Gravity telescopic tailstock and vertical take-off and landing tilting flat flight aircraft


    Weitere Titelangaben:

    一种重力可伸缩机尾座及垂直起降倾转平飞飞行器


    Beteiligte:
    ZHUO JIANFENG (Autor:in)

    Erscheinungsdatum :

    11.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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