The invention relates to a foldable all-moving film wing micro unmanned aerial vehicle, which comprises a motor bracket, the motor is mounted at the front part of the motor bracket; the nose is connected with the rear part of the motor bracket, and a propeller is mounted on the motor; the front folding mechanisms are arranged on the left side and the right side of the machine head, each front folding mechanism comprises a front folding frame and a front supporting rod connected with the front folding frame, and the front folding frames are fixed to the machine head; the machine body is adhered and fixed to the rear part of the machine head; the empennages are mounted on the left and right sides of the fuselage through empennage folding frames; the fuselage rear section is pivotally mounted to the rear part of the fuselage through a connecting pin; the steering engine is mounted in the rear fuselage section, and the rear part of the steering engine is connected with a steering engine rocker; the rear folding mechanisms extend from the steering engine rocker to the two sides respectively, each rear folding mechanism comprises a rear folding frame and a rear supporting rod connected with the rear folding frame, and the rear folding frames are connected with the steering engine rocker; and the film wings cover and are fixed on the lower surface of the fuselage, the front supporting rod and the rear supporting rod.

    一种可折叠全动薄膜机翼微型无人机,包括:电机支架;电机,安装至电机支架的前部;机头,与电机支架的后部连接,且电机上安装有螺旋桨;前折叠机构,设置在机头的左右两侧,该前折叠机构分别包括前折叠架以及与该前折叠架连接的前支撑杆,该前折叠架与机头固定;机身,粘接固定至机头的后部;尾翼,通过尾翼折叠架安装在机身的左右两侧;机身后段,通过连接销可枢转地安装至机身的后部;舵机,安装在所述机身后段中,且该舵机的后部连接有舵机摇杆;后折叠机构,分别从舵机摇杆向两侧延伸,且该后折叠机构分别包括后折叠架和与其连接的后支撑杆,该后折叠架与舵机摇杆连接;和薄膜机翼,覆盖并固定在机身下表面以及前支撑杆和后支撑杆上。


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    Title :

    Foldable all-moving film wing miniature unmanned aerial vehicle system


    Additional title:

    可折叠全动薄膜机翼微型无人机系统


    Contributors:
    HU TIANXIANG (author) / ZHOU MINGHAO (author) / LIN YOUSHEN (author) / LI JIAQI (author) / LU YING (author) / SU LIHANG (author) / QU QIULIN (author)

    Publication date :

    2022-04-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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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