Satellite on-orbit xenon supplementing system, working method and space flight equipment
Satellite on-orbit xenon supplementing system, working method and space flight equipment
- New search for: REN HAO
- New search for: ZHAO ZIYANG
- New search for: WANG XUAN
- New search for: XIAO KAIYANG
- New search for: GU YANGJIE
- New search for: LI WEIKUN
- New search for: SUN XIAOYI
- New search for: REN HAO
- New search for: ZHAO ZIYANG
- New search for: WANG XUAN
- New search for: XIAO KAIYANG
- New search for: GU YANGJIE
- New search for: LI WEIKUN
- New search for: SUN XIAOYI
The invention provides a satellite on-orbit xenon supplementing system, a working method and space flight equipment. The satellite on-orbit xenon supplementing system comprises a service star xenon bottle, a pressure reducing valve, a compressor, a compressor electromagnetic valve, a straight-through path electromagnetic valve and a target star xenon bottle. The service star xenon cylinder is connected with the target star xenon cylinder through a straight-through branch and a compressor supplementing branch which are connected in parallel; the straight-through branch is provided with a straight-through path electromagnetic valve, the compressor supplementing branch is provided with a pressure reducing valve, a compressor and a compressor electromagnetic valve, the service star xenon cylinder is connected with the straight-through path electromagnetic valve and the compressor electromagnetic valve, and the compressor electromagnetic valve is connected with the pressure reducing valve and the compressor in sequence. And the compressor and the straight path electromagnetic valve are connected with the target star xenon cylinder. According to the application, a xenon double-supplementing mode is adopted, direct-through supplementing can rapidly supplement the xenon, compressor supplementing can enable the xenon to be in a supercritical state, and the weight of the xenon supplemented by a target satellite is ensured.
本发明提供了一种卫星在轨氙气补加系统、工作方法及航天飞行设备，包括：服务星氙气瓶、减压阀、压缩机、压缩机电磁阀、直通路电磁阀以及目标星氙气瓶；所述服务星氙气瓶通过并联的直通支路和压缩机补加支路连接所述目标星氙气瓶；所述直通支路上设置有直通路电磁阀，所述压缩机补加支路上设置有减压阀、压缩机以及压缩机电磁阀，所述服务星氙气瓶分别连接所述直通路电磁阀和所述压缩机电磁阀，所述压缩机电磁阀先后连接减压阀和压缩机，所述压缩机和所述直通路电磁阀连接所述目标星氙气瓶。本申请采用氙气双补加模式，直通补加可快速补气，压缩机补加可使氙气处于超临界态，保证目标星补加的氙气重量。
Document information
Satellite on-orbit xenon supplementing system, working method and space flight equipment
卫星在轨氙气补加系统、工作方法及航天飞行设备
2024-03-29
Patent
Electronic Resource
Chinese
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