The invention relates to the technical field of aircraft assembly, and particularly discloses a pull rope fixing self-locking structure which comprises a pull rope, a pull rope adjusting assembly and a locking assembly, the pull rope is connected with a plug, the pull rope adjusting assembly is used for adjusting the slack amount of the pull rope, and the locking assembly is used for locking an adjusting rod of the pull rope adjusting assembly. The pull rope fixing and self-locking structure is mainly used on an aircraft, can well solve the problems that the risk is caused by the too large minimum looseness of the pull rope and the adjustment operation process of the minimum looseness is complex, and is simple in structure, convenient to operate and high in reliability.

    本申请涉及飞行器装配技术领域,具体公开了一种拉绳固定自锁结构,其包括拉绳,拉绳调节组件以及锁紧组件,其中,拉绳连接插头,拉绳调节组件用于对拉绳的松弛量进行调节,锁紧组件用于对拉绳调节组件的调节杆进行锁紧。该拉绳固定自锁结构主要用在飞行器上,拉绳固定自锁结构能够较好的解决拉绳的最小松弛量偏大带来的风险以及最小松弛量调整操作过程复杂的难题,结构简单、操作便利,可靠性高。


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    Titel :

    Stay rope fixing and self-locking structure


    Weitere Titelangaben:

    一种拉绳固定自锁结构


    Beteiligte:
    XIAO DETING (Autor:in) / JIN LEI (Autor:in) / FU ZHONGKUI (Autor:in) / WANG CHUNYAN (Autor:in) / HUANG JIN (Autor:in) / HUANG TUO (Autor:in) / LEI WEILIANG (Autor:in)

    Erscheinungsdatum :

    15.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    H01R Elektrisch leitende Verbindungen , ELECTRICALLY-CONDUCTIVE CONNECTIONS / B64G Raumfahrt , COSMONAUTICS



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