The invention provides a thermal control structure and a satellite comprising the thermal control structure. The thermal control structure comprises a pump assembly; the bypass assembly is communicated with the pump assembly through a pipeline; the thermal control assembly is respectively communicated with the pump assembly and the bypass assembly through pipelines; the radiation radiator is respectively communicated with the pump assembly and the bypass assembly through pipelines; the thermal control assembly comprises a first cabin plate, a second cabin plate, a third cabin plate and a fourth cabin plate; each of the first cabin plate, the second cabin plate, the third cabin plate and the fourth cabin plate comprises a plate body, and each plate body comprises an inlet and an outlet formed in the plate body and a fluid channel formed in the plate body; the inlet and the outlet are respectively communicated with the fluid channel; the fluid channel of the first cabin plate and the fluid channel of the second cabin plate are communicated with the pump assembly and the bypass assembly to form a first fluid loop; the fluid channel of the third deck and the fluid channel of the fourth deck are communicated with the pump assembly and the bypass assembly to form a second fluid loop.
本发明提供一种热控结构及包括该热控结构的卫星,该热控结构包括泵组件;通过管路与泵组件连通的旁路组件;通过管路分别与泵组件和旁路组件连通的热控组件;以及通过管路分别与泵组件和旁路组件连通的辐射散热器;热控组件包括:第一舱板、第二舱板、第三舱板和第四舱板;第一舱板、第二舱板、第三舱板和第四舱板均包括板体,板体包括形成于板体上的接入口和接出口,以及形成于板体内的流体通道;接入口和接出口分别与流体通道连通;第一舱板的流体通道和第二舱板的流体通道与泵组件和旁路组件连通形成第一流体回路;所述第三舱板的流体通道和第四舱板的流体通道与泵组件和旁路组件连通形成第二流体回路。
Thermal control structure and satellite comprising same
一种热控结构及包括该热控结构的卫星
2022-05-10
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
STRUCTURE DEPLOYING SYSTEM AND SATELLITE COMPRISING THE SAME
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