The invention relates to the technical field of satellite heat dissipation, and provides a satellite module heat dissipation system adopting liquid metal and an artificial satellite.The satellite module heat dissipation system adopting the liquid metal comprises a pipeline assembly, an electromagnetic pump, a thermoelectric module, an energy storage module and a radiator, the pipeline assembly is laid on the surface of a satellite module, and the liquid metal flows in the pipeline assembly; the electromagnetic pump is connected with the pipeline assembly to drive the liquid metal to flow; the thermoelectric module is connected with the outflow end of the pipeline assembly and used for generating electricity. The energy storage module is connected with the thermoelectric module, is used for storing electric energy and is electrically connected with the satellite module; the radiator is connected with the outflow end of the thermoelectric module and connected to the pipeline assembly through the electromagnetic pump. The heat dissipation requirement of high-power satellite equipment can be met, the satellite module can be installed in a severe environment, and electric energy stored by the energy storage module is supplied to the satellite equipment for use under extreme conditions.
本发明涉及卫星散热技术领域,提供一种采用液态金属的卫星模组散热系统和人造卫星,采用液态金属的卫星模组散热系统包括管路组件、电磁泵、热电模块、储能模块及散热器,管路组件平铺在卫星模组的表面,管路组件内流动有液态金属;电磁泵连接管路组件,以驱动液态金属流动;热电模块连接管路组件的流出端,热电模块用于发电;储能模块与热电模块连接,用于储存电能,储能模块与卫星模组电连接;散热器连接热电模块的流出端,散热器通过电磁泵连接至管路组件。本发明可以满足大功率卫星设备的散热需求,还能够将卫星模组安装于较为恶劣的环境中,储能模块储存的电能在极端条件下供给卫星设备使用。
Satellite module cooling system adopting liquid metal and artificial satellite
采用液态金属的卫星模组散热系统和人造卫星
2025-02-07
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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