The invention relates to an unfolding mechanism with linear and rotary two degrees of freedom. The unfolding mechanism comprises a base, an opening and closing assembly nested in the base and capable of sliding, and a linear motion driving part used for providing linear driving for the opening and closing assembly. The base comprises a hollow cylinder with one end open and the other end closed, and an annular limiting plate connected with the open end of the hollow cylinder; a limiting protrusion is arranged on the inner side face of the annular limiting plate. A first sliding limiting groove matched with the limiting protrusion is formed in the side face of the opening and closing assembly, and the bottom end of the first sliding limiting groove is closed. The linear motion driving part is used for driving the opening and closing assembly to stretch out in the linear direction till the bottom end of the first sliding limiting groove abuts against the limiting protrusion, and the opening and closing assembly is rotationally unfolded in the axial direction. The mechanism can be used for unfolding a structure on an aerospace craft, linear motion and rotary motion can be completed in sequence through one-time unlocking, motion locking is achieved, and the requirement for two-degree-of-freedom motion and locking can be met at the same time through one-time unlocking.

    本发明涉及一种具有线性和旋转双自由度的展开机构,包括:基座,嵌套在基座内且可滑动的开合组件,用于对开合组件提供线性驱动的直线运动驱动件;基座包括:一端开口且另一端封闭的中空柱体,与中空柱体的开口端相连接的环形限位板;环形限位板的内侧面设置有限位凸起;开合组件的侧面设置有与限位凸起相匹配的第一滑动限位槽,且第一滑动限位槽的底端封闭的设置;直线运动驱动件用于驱动开合组件沿直线方向伸出直至第一滑动限位槽的底端与限位凸起相抵靠,并且开合组件沿轴向旋转展开。本发明可用于航天飞行器上结构的展开,一次解锁就能先后完成直线运动和旋转运动并实现运动锁止,实现了一次解锁能同时满足两自由度运动与锁止的需求。


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    Title :

    Unfolding mechanism with linear and rotary two-degree-of-freedom


    Additional title:

    一种具有线性和旋转双自由度的展开机构


    Contributors:
    SU JIAN (author) / YE YUAN (author) / KANG IN-YONG (author) / WANG JIAYI (author) / NIE SHA (author) / WEN JUAN (author) / LIU QING (author) / SHAO ZHIQIANG (author) / YANG SHUN (author) / ZOU LU (author)

    Publication date :

    2024-03-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS



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