The embodiment of the invention provides a fixed-wing aircraft with a tilting duct. The aircraft comprises a left duct fan, a right duct fan, a tail duct fan, vertical tails, a middle lifting body, aleft empennage support rod and a right empennage support rod, the left duct fan and the right duct fan are respectively and correspondingly arranged at the end parts of a left wing and a right wing ofthe middle lifting body; both the left duct fan and the right duct fan can tilt around a spanwise shaft, the left empennage support rod and the right empennage support rod are correspondingly installed on the rear edges of the left wing and the right wing of the middle lifting body respectively, the vertical tails are fixedly arranged at the tails of the left empennage support rod and the right empennage support rod respectively, and the tail duct fan is installed between the opposite sides of the two vertical tails. The tail duct fan can tilt around the direction perpendicular to the vertical tails. The aircraft is concise and compact in layout and stable in structure, and can provide power and flight attitude control for vertical take-off and landing and high-speed cruise flight of theaircraft.

    本申请实施例提供了一种可倾转涵道的固定翼飞机,包括左涵道风扇、右涵道风扇、尾部涵道风扇、垂尾、中间升力体、左尾翼支撑杆和右尾翼支撑杆,所述中间升力体的左右翼端部分别对应安装有左涵道风扇和右涵道风扇,左涵道风扇和右涵道风扇均可绕展向轴倾转,中间升力体的左右翼身后边分别对应安装有左尾翼支撑杆和右尾翼支撑杆,左尾翼支撑杆和右尾翼支撑杆的尾部均固设有一垂尾,两垂尾相对侧之间安装有一尾部涵道风扇,尾部涵道风扇可绕垂直于垂尾方向倾转。本申请具有布局简洁紧凑、架构稳定且能为飞机在垂直起降和高速巡航飞行提供动力和飞行姿态控制。


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    Title :

    Fixed-wing aircraft with tiltable duct


    Additional title:

    一种可倾转涵道的固定翼飞机


    Contributors:
    SHEN LIANG (author) / YANG CHANGFA (author) / LENG ZHIHUI (author) / LIU MIN (author) / LI ZIQI (author) / FU WEIJIA (author) / HU ZHIDONG (author)

    Publication date :

    2021-02-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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