The embodiment of the invention discloses a course synergy system and a wing body fusion layout aircraft with the course synergy system. The course synergy system comprises a tail boom, an auxiliary engine, a vertical fin and a rudder. The tail boom is connected with the wing body fusion body and is internally provided with a containing cavity with two through ends. The auxiliary engine is located in a containing cavity of the tail boom, the vertical fin is connected with the tail boom, a ventilation pipeline communicated with an outer duct of the auxiliary engine is arranged in the vertical fin, the ventilation pipeline is provided with at least one air outlet extending to the surface of the vertical fin, and the rudder is movably connected with the vertical fin. When the aircraft takes off and lands, the auxiliary engine starts to work, air enters the outer duct and the inner duct of the auxiliary engine from the containing cavity, part of the air entering the outer duct also enters the ventilation pipeline and is sprayed out along an air outlet, located in the surface of the vertical fin, of the ventilation pipeline, and the flowing speed of surface airflow of the vertical fin can be increased; therefore, the control surface efficiency of the rudder is improved, and the course control capability is improved.

    本申请实施例公开了一种航向增效系统及具有航向增效系统的翼身融合布局飞行器。该航向增效系统包括尾撑、辅助发动机、垂尾及方向舵。尾撑连接翼身融合体,尾撑中具有两端贯穿的容纳腔。辅助发动机位于尾撑的容纳腔中,垂尾与尾撑连接,垂尾中具有与辅助发动机的外涵道连通的通气管道,通气管道上具有延伸至垂尾的表面的至少一个出气口,方向舵与垂尾活动连接。在飞行器起飞和降落阶段时,辅助发动机开始工作,空气从容纳腔中进入辅助发动机的外涵道和内涵道,进入外涵道的空气的一部分也会进入通气管道中,并沿通气管道位于垂尾表面的出气口喷出,可以加快垂尾的表面气流的流动速度,以提高方向舵的舵面效率,增加航向控制能力。


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    Title :

    Course synergy system and wing body fusion layout aircraft with course synergy system


    Additional title:

    航向增效系统及具有航向增效系统的翼身融合布局飞行器


    Contributors:
    WU DAWEI (author) / YANG HAIPENG (author) / MA RUBING (author) / PI ZHENGYANG (author) / CHENG CHANGFU (author) / LIANG JUN (author)

    Publication date :

    2022-01-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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