The invention belongs to the technical field of aircrafts, and particularly discloses a variant fixed-wing aircraft with foldable wings, which comprises an aircraft body, the wings are arranged on one side of the aircraft body, a first fixing rod is fixedly connected to the inner wall of the aircraft body, a first fixing frame is arranged on one side, close to the aircraft body, of each wing, and the first fixing frame is L-shaped; the side, close to the first fixing rod, of the first fixing frame is rotationally connected with the surface of the first fixing rod, and the side, away from the first fixing rod, of the first fixing frame is rotationally connected with a first transmission rod. When the aircraft is folded backwards, a sliding table is driven to move and drives a first connecting rod and a first transmission rod to rotate, so that a first fixing frame rotates on a first fixing rod, the wings are folded backwards, and the gravity center position of the aircraft is actively controlled through longitudinal movement of a sliding rail in the aircraft body.

    本发明属于飞行器技术领域,具体公开了一种可以折叠机翼的变体式固定翼飞行器,包括机体,机体的一侧设置有机翼,所述机体的内壁固定连接有第一固定杆,机翼靠近机体的一侧设置有第一固定架,第一固定架为L形,第一固定架靠近第一固定杆的一侧与第一固定杆的表面转动连接,第一固定架远离第一固定杆的一侧转动连接有第一传动杆,该可以折叠机翼的变体式固定翼飞行器,通过外部控制装置使第一电机启动,第一电机在第一固定架的限制下,带动滑台进行移动,并使滑台带动第一连接杆与第一传动杆进行转动,从而使第一固定架在第一固定杆上进行转动,从而实现机翼的向后折叠,利用机身内滑轨的纵向移动主动控制飞行器重心位置。


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    Title :

    Variant type fixed-wing aircraft with foldable wings


    Additional title:

    一种可以折叠机翼的变体式固定翼飞行器


    Contributors:
    HE XINRUI (author) / CHENG ZIJUN (author) / ZHANG MUYUE (author) / ZHAO YICHAO (author) / MA MINGZHE (author) / ZHU HAONAN (author) / LAO ZILU (author) / ZHANG TIANPENG (author) / YANG ZHAOJUN (author) / TONG WENJING (author)

    Publication date :

    2023-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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