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A HEAT PUMP FOR SPACE APPLICATIONS WITH A LIGHTWEIGHT 200,000 RPM CENTRIFUGAL THREE-STAGE COMPRESSOR SYSTEM

机译:轻型200,000 RPM离心三级压缩机系统的空间应用的热泵

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摘要

Satellites have to reject waste heat into space with radiators. These radiators largely determine the size of the satellite, and a further increase in radiator size to increase the heat rejection capacity is not practical. The heat rejection capacity can also be increased by using a heat pump to increase the radiator temperature of the satellite. However, traditional compressors are too heavy (40 kg) and cause too much vibrations. For this reason, a heat pump demonstrator with a lightweight (2 kg), low-vibration, centrifugal three-stage compressor system has been developed in a project funded by the European Space Agency (ESA). Tests were carried out with the heat pump, and the measured Coefficient of Performance (COP) is 2.3, which is higher than the ESA requirement of 2. The measured isentropic efficiency of the compressor is 68%, which is higher than existing aerospace compressors and even higher than some commercially available scroll compressors.
机译:卫星必须通过散热器将废热排入太空。这些辐射器在很大程度上决定了卫星的尺寸,并且进一步增加辐射器尺寸以增加散热能力是不切实际的。散热能力也可以通过使用热泵来提高卫星的散热器温度来提高。但是,传统的压缩机太重(40千克),并且会引起过多的振动。因此,在由欧洲航天局(ESA)资助的项目中,开发了一种具有轻量级(2 kg),低振动,离心式三级压缩机系统的热泵演示器。使用热泵进行测试,测得的性能系数(COP)为2.3,高于ESA要求2。测得的压缩机等熵效率为68%,高于现有的航空压缩机和甚至高于某些商用涡旋压缩机。

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