The invention provides a high-bearing thin wing type trailing edge control surface and fixed wing surface assembly for an unmanned aerial vehicle and a mounting method thereof, and can solve the problems that the weight of a fixed wing surface is increased due to the fact that the tip of the fixed wing surface needs to bear a large load when the trailing edge control surface bears a large load, and the rear extending part of the tip of the fixed wing surface occupies the area of the trailing edge control surface; and the control efficiency is low. The assembly comprises a trailing edge control surface, a fixed wing surface and two dimensional patch assemblies, the trailing edge control surface comprises a control surface beam, a skin and two control surface lugs, a first boss is arranged on the control surface beam, each control surface lug comprises a transverse plate, a double-lug, a second boss and a connecting piece, the transverse plate is connected with the control surface beam through the connecting piece, and the double-lug is arranged on the skin. The skin covers a combination body formed by the control surface beam and the control surface lugs, the fixed wing surface is provided with two wing surface lugs hinged to the two double lugs respectively, and during hinging, patch filling spaces used for installing a maintenance patch assembly are formed among the transverse plate, the first boss corresponding to the transverse plate, the second boss corresponding to the transverse plate and the fixed wing surface.

    本发明提供了无人机用高承载薄翼型后缘舵面与固定翼面组合件及其安装方法,能解决后缘舵面承载较大时因需要固定翼面稍部承受较大载荷,导致固定翼面增重,及固定翼面稍部的后延部分因占用后缘舵面面积,导致操纵效率低的问题。该组合件包括后缘舵面、固定翼面及两个维型补块组件,后缘舵面包括舵面梁、蒙皮及两个舵面耳片,舵面梁上设有第一凸台,舵面耳片包括横板、双耳片、第二凸台及连接件,横板通过连接件与舵面梁连接,蒙皮包覆在舵面梁及舵面耳片构成的组合体外,固定翼面上设有分别与两个双耳片铰接的两个翼面耳片,铰接时,在横板和与其对应的第一凸台、第二凸台及固定翼面之间构成用于安装维型补块组件的补块填充空间。


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    Title :

    High-bearing thin wing type trailing edge control surface and fixed wing surface assembly for unmanned aerial vehicle and mounting method thereof


    Additional title:

    无人机用高承载薄翼型后缘舵面与固定翼面组合件及其安装方法


    Contributors:
    HU WEI (author) / LI HONGSHENG (author) / LI HONGJUN (author) / FENG XIAOQIANG (author) / HE YANG (author) / YANG WENCHONG (author) / GAO XIN (author)

    Publication date :

    2024-11-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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