The invention discloses a multi-attitude duct control system and an aircraft, the multi-attitude duct control system comprises a duct ring body, a power propeller is erected in the duct ring body, and a telescopic turbulent flow assembly is arranged on the inner wall of the duct ring body; the telescopic turbulent flow assembly comprises a sliding groove and a turbulent flow plate. A sliding groove is formed in the inner wall of the duct ring body, a spoiler is arranged in the sliding groove in a sliding mode, and the duct ring body is connected with the spoiler through a linear moving mechanism. According to the telescopic spoiler assembly, in the single-duct aircraft, the local flow field in the single duct is changed through the telescopic spoiler, then the local lift force in a single-duct system is changed, and finally the single duct has the vector action function. The telescopic turbulent flow assembly can be used in a multi-duct aircraft in a linkage mode, and the vector action and the flight attitude of the whole aircraft are changed.

    本发明公开了一种多姿态涵道控制系统及飞行器,包括涵道圈体,所述涵道圈体内架设动力螺旋桨,所述涵道圈体内壁设置伸缩扰流组件;所述伸缩扰流组件包括滑槽、扰流板;所述涵道圈体内壁设置滑槽,所述滑槽内滑动设置扰流板,所述涵道圈体与扰流板通过直线移动机构连接。本发明设置的伸缩扰流组件在单涵道飞行器中,通过伸缩扰流板改变单涵道内的局部流场,进而改变单涵道系统内的局部升力,最终使单涵道具备矢量动作功能。本发明设置的伸缩扰流组件在多涵道飞行器中,可联动使用,改变整体飞行器的矢量动作,及飞行姿态。


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    Title :

    Multi-attitude duct control system and aircraft


    Additional title:

    一种多姿态涵道控制系统及飞行器


    Contributors:
    ZHENG WEI (author)

    Publication date :

    2025-04-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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