The invention relates to aero-engine assembly auxiliary equipment, and relates to the technical field of aero-engines, the auxiliary equipment comprises a mounting seat, a lifting hook mechanism is arranged on the mounting seat, and auxiliary stabilizing mechanisms are arranged on the two opposite sides of the lifting hook mechanism; the auxiliary stabilizing mechanism comprises an extension arm, a pushing arm and a clamping jaw, the extension arm is arranged in the vertical direction, the pushing arm is arranged at the lower end of the extension arm and arranged in the horizontal direction, the clamping jaw is arranged at the end, facing the lifting hook mechanism, of the pushing arm, and the pushing arm comprises a pushing driving part capable of pushing the clamping jaw to move in the horizontal direction. The auxiliary clamping mechanisms are arranged on the two sides of the lifting hook mechanism, a part lifted by the lifting hook mechanism is reinforced in the horizontal direction through the clamping jaws, and the shaking condition of the lifted part in the mounting process can be reduced.

    本申请涉及一种航空发动机装配辅助设备,涉及航空发动机的技术领域,辅助设备包括安装座,安装座上设置有吊钩机构,吊钩机构相对两侧均设置有辅助稳定机构;辅助稳定机构包括伸长臂、推动臂和夹爪,伸长臂沿竖直方向设置,推动臂设置在伸长臂下端且推动臂沿水平方向设置,夹爪设置在推动臂朝向吊钩机构的一端,推动臂包括能够推动夹爪沿水平方向运动的推动驱动件。本申请在吊钩机构的两侧设置辅助夹持机构,通过夹爪对吊钩机构吊起的零件进行水平方向的加固,能够降低吊起的零件在安装过程之中的晃动情况。


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    Titel :

    Aero-engine assembly auxiliary equipment


    Weitere Titelangaben:

    一种航空发动机装配辅助设备


    Beteiligte:
    ZHOU DONGDONG (Autor:in)

    Erscheinungsdatum :

    2023-10-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B66C Krane , CRANES



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