The invention belongs to the technical field of aviation, and particularly relates to an auxiliary flight device for a composite wing aircraft, which comprises wings on the two sides of the composite wing aircraft, and is characterized in that exhaust holes are formed in the wings on the two sides, connecting pipes communicated with the exhaust holes are mounted on the exhaust holes, and the connecting pipes are fixed in the wings; a high-pressure air source is mounted at the other end of the connecting pipe, and a valve is mounted on the connecting pipe; the valve can be mounted at any position on the connecting pipe and comprises an end part of the connecting pipe; the high-pressure air source is mounted on the aircraft; and the position of the exhaust hole is close to the wing tip of the wing. The method has the following beneficial effects that when the aircraft rolls, the flight attitude of the aircraft can be corrected in time, so that the aircraft can fly stably.

    本发明属于航空技术领域,尤其涉及一种复合翼飞行器辅助飞行装置,包括复合翼飞行器的两侧机翼,其特征在于:两侧所述机翼上开设有排气孔,所述排气孔上安装有与其连通的连接管,所述连接管固定于机翼内部,所述连接管的另一端安装有高压气源,所述连接管上安装有阀门;所述阀门可安装在连接管上的任一位置,包括连接管的端部;所述高压气源安装在飞行器上;所述排气孔的位置靠近机翼的翼尖。本发明具有以下有益效果:可以在飞行器发生滚转时,及时地矫正飞行器的飞行姿态,使得飞行器能够平稳飞行。


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    Title :

    Auxiliary flight device of composite wing aircraft


    Additional title:

    一种复合翼飞行器辅助飞行装置


    Contributors:
    YU YANG (author) / YANG YALIN (author) / YANG LI (author) / LIANG SIJIA (author) / YU TAO (author) / LI RUIZHE (author)

    Publication date :

    2022-05-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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