The invention discloses a rocket cabin lifting device which comprises a connecting rod assembly, a lifting rod assembly, a lifting rod assembly, a lifting rod assembly, a lifting rod assembly, a lifting rod assembly, a lifting rod assembly and a lifting rod assembly, and the connecting rod assembly is provided with an operating end and two clamping ends; when the connecting rod assembly is in a natural state, a set distance is formed between the two lifting lugs, and the set distance is not smaller than the interval between the two ends of a rocket cabin. When vertical upward traction force is applied to the operation end of the connecting rod assembly, the two clamping ends of the connecting rod assembly get close to each other so as to drive the two lifting lugs to clamp the two ends of the rocket cabin, and the two lifting lugs are in a clamping state. According to the rocket cabin hoisting device, the efficiency of rocket cabin hoisting work can be improved.

    本申请公开了一种火箭舱体吊运装置,包括:连杆组件,所述连杆组件具有操作端和两个加持端,所述加持端上连接有吊耳;当所述连杆组件处于自然状态时,两个所述吊耳之间具有设定间距,所述设定间距不小于火箭舱体两端的间隔;当向所述连杆组件操作端施加竖直向上的牵引力时,所述连杆组件的两个所述加持端相互靠近,以驱动两个所述吊耳对所述火箭舱体的两端形成加持,并处于加持状态。该火箭舱体吊运装置可提升对火箭舱体吊运工作的效率。


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    Titel :

    Rocket cabin hoisting device


    Weitere Titelangaben:

    一种火箭舱体吊运装置


    Erscheinungsdatum :

    24.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B66C Krane , CRANES



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