The invention discloses a separation device, belongs to the technical field of spacecraft and rocket separation, and aims at solving the problems that an existing traditional satellite and rocket connection and separation device is tedious in design layout, variable in interface form, complex in installation operation, low in design efficiency, heavy in weight and the like. The separation device provided by the embodiment of the invention is used for separating a first component from a second component, and comprises a pushing frame, the guide assembly is arranged on one side of the pushing frame and movably connected with the pushing frame; the pushing assembly is fixedly connected with the pushing frame and can provide pushing force to enable the pushing frame to move in the guiding direction of the guiding assembly, the first component is pushed to move in the direction away from the second component, and therefore the first component and the second component are separated.
本申请公开了一种分离装置,属于航天器星箭分离的技术领域,以解决目前传统的星箭连接分离装置存在设计布局繁琐、接口形式多变、安装操作复杂、设计效率低下、星箭连接分离装置重量较重等问题。本申请实施例提供的一种分离装置,用于分离第一构件和第二构件,包括:顶推框;导向组件,设置于顶推框一侧且与所述顶推框活动连接;顶推组件,与所述顶推框固定连接,能够提供推力使所述顶推框沿所述导向组件的导向方向运动,推动所述第一构件向远离所述第二构件的方向运动,以使所述第一构件和所述第二构件分离。
Separating device
分离装置
2023-10-03
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |