The invention provides a rope-driven telescopic swing rod lifting and transferring device and a transferring method, and belongs to the technical field of planet patroller transferring mechanisms. The problems that the transfer mechanism and the planet patroller are separated from and unlocked from the lander, how to enable the transfer mechanism to reliably transfer the planet patroller to the lunar surface and can reliably transfer the planet patroller to the lunar surface under various landing working conditions are solved, and the lunar landing place of the planet patroller has a certain selectable range, so that the planet patroller can be reliably transferred to the lunar surface. And a plurality of technical problems of pits and bulges on the lunar surface are solved. The device comprises a separating mechanism, a telescopic swing rod, a front arm and a swing rod releasing mechanism, one end of the telescopic swing rod is fixed on a lander, the other end of the telescopic swing rod is connected with the front arm, the front arm is connected with a planet patrolling device through the separating mechanism, and the swing rod releasing mechanism is fixed on the side wall of the lander, provides power for the action of the telescopic swing rod and completes stretching and releasing. The releasing position suitable for landing of the planet patroller can be selected at will within the linear range, and landing is flexible.

    本发明提出了一种绳驱伸缩摆杆托举转移装置和转移方法,属于星球巡视器转移机构技术领域。解决了转移机构及星球巡视器实现与着陆器的分离解锁,如何使转移机构将星球巡视器可靠转移至月面,且能在各种着陆工况下,均可实现将星球巡视器可靠转移至月面,以及星球巡视器落月地点应具有一定可选范围,以避开月面凹坑和凸起的多个技术问题。它包括脱离机构、伸缩摆杆、前臂和摆杆释放机构,伸缩摆杆一端固定在着陆器上,另一端与前臂连接,前臂通过脱离机构与星球巡视器连接,摆杆释放机构固定于着陆器侧壁,为伸缩摆杆的作动提供动力,完成伸缩和释放。本发明能够在直线范围内任意选择适合星球巡视器着陆的释放位置,着陆灵活。


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    Titel :

    Rope-driven telescopic swing rod lifting and transferring device and method


    Weitere Titelangaben:

    一种绳驱伸缩摆杆托举转移装置和转移方法


    Beteiligte:
    YANG ZHILUN (Autor:in) / LI JIANYONG (Autor:in) / ZHOU XIAOLONG (Autor:in) / WANG YINCHAO (Autor:in) / TANG JUNYUE (Autor:in) / ZHANG WEIWEI (Autor:in) / YANG FEI (Autor:in) / JIANG SHENGYUAN (Autor:in) / DENG ZONGQUAN (Autor:in)

    Erscheinungsdatum :

    07.04.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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