The invention relates to a holding claw type on-orbit detachable pressing and releasing mechanism, and belongs to the field of pressing and releasing of spacecraft mechanisms. Comprising a captive screw, a first sliding block, a pressing cap, a holding claw, a first support, a second sliding block, a compression spring, a spring sleeve, a pressing head sleeve, a locknut, a loading nut, a force bearing bowl, a tension spring, a long screw rod, a second support and a pressed part. The working process of the pressing and releasing mechanism comprises the three stages of long screw rod releasing, holding claw holding and pressing and releasing mechanism on-orbit dismounting. And finally, the astronaut integrally takes away the pressing and releasing mechanism and places the pressing and releasing mechanism in a storage bag, and the on-orbit dismounting work of the pressing and releasing mechanism is completed. According to the invention, astronaut on-orbit disassembly can be realized, and the claw type structure is adopted to tightly hold internal parts to realize disassembly, assembly and separation without scattering, and no space debris is generated.
本发明涉及一种抱爪式在轨可拆卸压紧释放机构,属于航天器机构的压紧释放领域;包括松不脱螺钉、第一滑块、压紧帽、抱爪、第一支架、第二滑块、压缩弹簧、弹簧套管、压紧头套、防松螺母、加载螺母、承力碗、拉簧、长螺杆、第二支架和被压件;压紧释放机构的工作过程包括长螺杆释放、抱爪抱紧、压紧释放机构在轨拆卸3个阶段;最终航天员将压紧释放机构整体拿走放置在收纳袋中,完成压紧释放机构在轨的拆卸工作;本发明可以实现航天员在轨拆卸,该方案采用爪式结构抱紧内部零件实现拆装分离且不散落、不产生空间碎片。
Claw type on-orbit detachable pressing and releasing mechanism
一种抱爪式在轨可拆卸压紧释放机构
2023-05-16
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
On-orbit detachable large solar wing pressing and releasing mechanism
European Patent Office | 2023
|High-reliability holding claw type on-orbit filling mechanism and method
European Patent Office | 2024
|Pressing and releasing mechanism and releasing method for stacked satellites
European Patent Office | 2023
|Open type tail cover solar wing pressing and releasing mechanism
European Patent Office | 2023
|