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作者:

Ma, Rui (Ma, Rui.) | Wu, Yuting (Wu, Yuting.) (学者:吴玉庭) | Liu, Gang (Liu, Gang.) | Ma, Chongfang (Ma, Chongfang.)

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摘要:

Vapor compression heat pump has a good prospect of application in high temperature environments and high-power spacecraft thermal control system. Aerospace vapor compression heat pump operates in the microgravity environment. Microgravity vapor compression heat pump adaptability is the key to a vapor compression heat pump technology aerospace research and development. The evaporator is a key component of the vapor compression heat pump. By calculating vapor compression heat pump evaporator to explore its gravity-independent conditions and get gravity-independent critical velocity and critical diameter at different evaporation temperatures and under different flow rates. The results showed that the minimum critical velocity in the evaporator gravity-independent region in 1.45-1.5 m·s-1. The maximum critical diameter increases with cooling capacity, and cooling capacity from 50 W to 300 W, the critical diameter from 0.42 mm to 1.02 mm. © All Rights Reserved.

关键词:

Cooling Evaporators Heat pump systems Microgravity Microgravity processing Pumps

作者机构:

  • [ 1 ] [Ma, Rui]Environment and Energy Engineering, Beijing University of Technology, Beijing 100124, China
  • [ 2 ] [Wu, Yuting]Environment and Energy Engineering, Beijing University of Technology, Beijing 100124, China
  • [ 3 ] [Liu, Gang]Environment and Energy Engineering, Beijing University of Technology, Beijing 100124, China
  • [ 4 ] [Ma, Chongfang]Environment and Energy Engineering, Beijing University of Technology, Beijing 100124, China

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来源 :

CIESC Journal

ISSN: 0438-1157

年份: 2014

期: SUPPL.1

卷: 65

页码: 125-129

被引次数:

WoS核心集被引频次: 0

SCOPUS被引频次: 3

ESI高被引论文在榜: 0 展开所有

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