The invention discloses a swing sliding type flapping rotor device, which is characterized in that main shafts are arranged on two sides of a fuselage through flapping rotor wing brackets and are rotationally connected with the flapping rotor wing brackets through bearings, and the axial center lines of the main shafts are parallel to the axial center line of the fuselage; the center of the bottomof the swing arm is rotationally connected to the main shaft through a rotating shaft, and meanwhile the linear driving device is installed on the swing arm and electrically connected with the controller. Rotor types of the rotors are symmetrical biconvex wings, a center hole is formed in the center of the rotary disc, a center shaft penetrates through the center hole and is rotationally connected with the rotary disc through a bearing, meanwhile, the center shaft is connected to a linear driving device, the linear driving device drives the center shaft to slide on the swing arm in a reciprocating mode, and the swing arm swings relative to the main shaft through a rotary shaft. The invention discloses the swing sliding type flapping rotor device. The efficiency and the size of lift forcegeneration are improved.

    本发明公开了一种摇摆滑动式扑旋翼装置,主轴通过扑旋翼支架设置在机身的两侧,并通过轴承与扑旋翼支架转动连接,且主轴的轴向中心线与机身的轴向中心线平行;摆动臂的底部中心处通过转轴转动连接在主轴上,同时,直线驱动装置安装在摆动臂上,并与控制器电性连接;旋翼的转动翼型为对称双凸翼型,转盘的中心开设有中心孔,中心轴穿过中心孔并通过轴承与转盘转动连接,同时中心轴连接在直线驱动装置上,直线驱动装置驱动中心轴在摆动臂上往复滑动,则摆动臂通过转轴相对主轴摆动。本发明公开了一种摇摆滑动式扑旋翼装置,提高了升力产生的效率和大小。


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    Title :

    Swing sliding type flapping rotor device


    Additional title:

    一种摇摆滑动式扑旋翼装置


    Contributors:

    Publication date :

    2021-03-02


    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



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