The invention relates to a four-bar mechanism for flight platform attitude control, the four-bar mechanism is mounted on a flight platform, the four-bar mechanism comprises a support frame, a steering engine is mounted at the top of the support frame, the steering engine is connected with an external power supply, the steering engine is connected with a steering engine arm, the steering engine arm is connected with a transmission rod, the transmission rod is connected to a lug piece, and the lug piece is connected with the support frame. The lug is connected with a fixing frame, a turbojet engine is installed on the fixing frame, and the fixing frame is connected with a bearing installed on the supporting frame. Compared with the prior art, the attitude control precision of the flight platform can be effectively improved, and the construction cost is reduced.

    本发明涉及一种用于飞行平台姿态控制的四连杆机构,安装于飞行平台,所述四连杆机构包括支撑架,所述支撑架的顶部安装有舵机,所述舵机与外部电源连接,所述舵机连接有舵机臂,所述舵机臂与传动杆连接,所述传动杆连接至耳片,所述耳片与固定架连接,所述固定架上安装有涡喷发动机,所述固定架与安装在支撑架上的轴承相连接。与现有技术相比,本发明能够有效提高飞行平台的姿态控制精度,降低构造成本。


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    Titel :

    Four-bar mechanism for flight platform attitude control


    Weitere Titelangaben:

    一种用于飞行平台姿态控制的四连杆机构


    Beteiligte:
    TANG WAN (Autor:in) / CHEN SAIXUAN (Autor:in) / QI XUERUI (Autor:in) / ZHENG JIALE (Autor:in) / CUI GUOHUA (Autor:in) / YAO BAIQIANG (Autor:in)

    Erscheinungsdatum :

    2022-08-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16C SHAFTS , Wellen



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