The performance of the thermoelectricheatpump low-temperature water heater was investigated under various operating conditions.
对一台空气源热电热泵低温热水装置在不同工作条件下的性能进行了实验研究。
2
The results indicate that the mini thermoelectricheatpump-PCM thermal control system can provide effective thermal control of high power spacecraft electronics.
结果表明,采用该热控系统对航天器短时大功率组件进行温度控制是可行的。
3
A novel instantaneous water heater was developed by means of integrating a thermoelectric(TE) heat-pump with a separating thermo-siphon.