The invention discloses an airplane gravity center automatic adjusting seat structure. The seat structure comprises a fuselage and an undercarriage, wherein the fuselage is connected with the undercarriage; a seat is arranged in the fuselage, and a sliding mechanism is arranged at the bottom of the seat; and a sensor is arranged at the bottom of the undercarriage, a controller and an absolute value encoder are further arranged in the fuselage, the absolute value encoder is connected with the controller, and the controller makes the sliding mechanism act according to signals fed back by the sensor and the absolute value encoder so as to make the seat be adjusted front and back. The airplane gravity center automatic adjusting seat structure solves technical problems that existing airplane gravity center adjusting is complex in structure, inconvenient to operate and insufficient in adjusting precision.

    本申请公开了一种飞机重心自动调节座椅结构。该座椅结构包括:机身和起落架,所述机身与所述起落架连接;所述机身内设置有座椅,所述座椅底部设置有滑动机构;所述起落架底部设置有传感器,所述机身内还设置有控制器和绝对值编码器,所述绝对值编码器与所述控制器连接,所述控制器根据所述传感器和所述绝对值编码器反馈的信号,控制所述滑动机构动作,进而控制座椅前后调节。本申请解决了现有的飞机重心调节存在结构复杂,操作不便和调节精度不足的技术问题。


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    Titel :

    Airplane gravity center automatic adjusting seat structure


    Weitere Titelangaben:

    一种飞机重心自动调节座椅结构


    Beteiligte:
    WANG YONG (Autor:in)

    Erscheinungsdatum :

    2020-10-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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