The invention relates to a connection and separation mechanism for stacked satellites, and belongs to the field of stacked satellites, the connection and separation mechanism comprises supporting plates arranged on the peripheral sides of the satellites, two supporting rods are arranged on the supporting plates on the same side of the satellites in a penetrating mode, limiting blocks are arranged at the ends, away from each other, of the two supporting rods, and the two limiting blocks abut against the supporting plates at the two ends respectively; the ends, close to each other, of the two supporting rods are connected together in a threaded mode, the supporting plate is provided with a separation assembly used for enabling the two supporting rods to be loosened and separated, in the using process, under the action of the separation assembly, the two supporting rods are loosened and separated, then the stacked satellites can be separated, the possibility that the satellites are damaged is reduced, and the separation success rate is increased.
本申请涉及一种堆叠式卫星的连接分离机构,属于堆叠式卫星领域,包括:设于卫星周侧的支板,位于所述卫星同侧的支板上穿设有两支杆,两所述支杆相远离的一端均设有限位块,两所述限位块分别抵接于两端的支板上,两所述支杆相靠近的一端螺纹连接在一起,所述支板上设有用于使两支杆松脱分离的分离组件,本申请在使用时,在分离组件的作用下,两支杆松脱分离,即可使堆叠式卫星分离,降低了卫星受损的可能性,提升了分离的成功率。
Connection and separation mechanism of stacked satellites
一种堆叠式卫星的连接分离机构
2024-02-06
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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