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VACUUM ›› 2020, Vol. 57 ›› Issue (2): 62-65.doi: 10.13385/j.cnki.vacuum.2020.02.12

• Measurement and Control • Previous Articles     Next Articles

Design and Analysis of Temperature Control Heat Sink for Thermal Vacuum Test Equipment

QI Song-song1, XU Xiao-hui2, LIU Jia-lin1, ZHANG Rui1, LI Can-lun1, DONG De-sheng1, SHI Cheng-tian1   

  1. 1.Shanghai Institute of spacecraft Equipment, Shanghai 200240, China;
    2.Shanghai Academy of Spaceflight Technology, Shanghai 200240, China
  • Received:2019-12-09 Online:2020-03-25 Published:2020-04-24

Abstract: In order to meet the thermal vacuum test requirements of a certain aerospace product, a special temperature-controlled heat sink is designed, which consists of a heat sink, a heater and a supporting temperature control system. This paper briefly describes the design of a special temperature control heat sink for a certain product, and carries out simulation analysis and verification of the structure. The analysis results show that, when the product heat is 200W, the space temperature can be higher than +120℃, the heat sink body temperature can be lower than-180℃, with temperature control conditions. The temperature control system adopts PID adaptive adjustment. The results show that the space temperature can be controlled from -180℃ to +120℃, and the temperature control accuracy can reach ±0.5℃, which meets the test requirements.

Key words: thermal vacuum test, temperature control heat sink, simulation analysis, PID control

CLC Number: 

  • V416.5
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