The invention provides an aircraft anti-load seat. The aircraft anti-load seat comprises a base, a rotary table assembly, a hydraulic cylinder assembly and a hollow seat. Mercury is packaged in the base; the rotary table assembly is mounted on the base, and a rotary table rotates horizontally; and the bottom of the hydraulic cylinder assembly is fixedly connected with the rotary table assembly, and the top of the hydraulic cylinder assembly is fixedly connected with the hollow seat. According to the aircraft anti-load seat, the problem that an existing aircraft seat does not weaken an acceleration load is well solved.

    本发明提供了一种飞行器抗载荷座椅,包括:底座、旋转转台组件、液压缸组件以及镂空座椅;所述底座内部封装水银;所述旋转转台组件安装在底座上,所述旋转转台作水平旋转运动;所述液压缸组件的底部与所述旋转转台组件相固接,所述液压缸组件的顶部与所述镂空座椅相固接。本发明提供的飞行器抗载荷座椅,很好地解决现有飞行器座椅不具备削弱加速度载荷的问题。


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    Titel :

    Aircraft anti-load seat


    Weitere Titelangaben:

    一种飞行器抗载荷座椅


    Beteiligte:
    CUI KAI (Autor:in) / CUI YINGQI (Autor:in) / LI JING (Autor:in)

    Erscheinungsdatum :

    2021-05-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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