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Liquid nitrogen and cold helium double media coupling heat sink for space environment simulation

A dual-medium, coupled heat technology, applied in household refrigeration devices, applications, household appliances, etc., can solve the problems of high temperature environment conditions that cannot be achieved above normal temperature, expensive liquid helium, high production cost, etc., to achieve good thermal conductivity, Effects of easy separation, good low temperature and corrosion resistance

Active Publication Date: 2013-11-13
SHANGHAI JIAO TONG UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the high price of liquid helium, the system is not only expensive to manufacture but also expensive to operate, so it is not suitable for long-running tasks such as survivability tests, and this heat sink cannot achieve high-temperature environmental conditions above normal temperature

Method used

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  • Liquid nitrogen and cold helium double media coupling heat sink for space environment simulation
  • Liquid nitrogen and cold helium double media coupling heat sink for space environment simulation
  • Liquid nitrogen and cold helium double media coupling heat sink for space environment simulation

Examples

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Embodiment Construction

[0026] The liquid nitrogen-cooled helium dual-medium coupling heat sink of the present invention is a closed cylinder, including a liquid nitrogen cooling pipe network, a cold air helium cooling pipe network, copper fins, an electric heater and a gas nitrogen blowing system, and the copper fins are connected to the liquid The nitrogen cooling pipe network and the cold air helium cooling pipe network form a heat sink cylinder together with the liquid nitrogen cooling pipe network and the cold air helium cooling pipe network. The two end faces of the heat sink (the first end face and the second end face) Covering the sealing plate of the end face, electric heaters are evenly distributed on the copper fins.

[0027] figure 1 It shows the liquid nitrogen cooling pipe network and the cold gas helium cooling pipe network in the liquid nitrogen-cooled helium dual-medium coupled heat sink of the present invention in a preferred embodiment. Such as figure 1 As shown, in this embodime...

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Abstract

The invention discloses a liquid nitrogen and cold helium double media coupling heat sink for space environment simulation. The heat sink is a sealed cylinder which comprises a liquid nitrogen cooling pipe network, a cold air helium cooling pipe network, copper fins and electric heaters, wherein the copper fins are connected with the liquid nitrogen cooling pipe network and the cold air helium cooling pipe network and forms a barrel of the liquid nitrogen and cold helium double media coupling heat sink with the liquid nitrogen cooling pipe network and the cold air helium cooling pipe network. The electric heaters are uniformly distributed on the copper fins. According to the heat sink disclosed by the invention, the liquid nitrogen cooling pipe network and the cold air helium cooling pipe network are embedded and coupled, so that refrigerating media liquid nitrogen and cold helium work independently to switch in function smoothly, thereby, realizing transition from a liquid nitrogen temperature area to a low temperature gas helium temperature area. In addition, according to design of two parallel and staggered medium pipelines with two runners, conditions of complex flow, reduced safety, discontinuous transition of the temperature area and waste of cooling capacity caused by emptying switch of a single runner can be avoided. The heat sink disclosed by the invention is simple in operational flow and safe and reliable.

Description

technical field [0001] The invention relates to a heat sink, in particular to a liquid nitrogen-cooled helium double-medium coupled heat sink for space environment simulation. Background technique [0002] The space environment simulation system simulates the vacuum and cold dark environment of the universe. It is an important equipment for testing the safety and reliability of aerospace equipment and its components in the space environment. The environment simulation cabin is the core component of the system. In addition to the shell and heat insulation methods in the environmental simulation cabin, the cold and heat sources in the cabin are generally completed through the heat sink. The heat sink provides the required temperature environment for the equipment under test through radiation heat transfer and other forms. To achieve this purpose, the temperature of the heat sink must be controlled. The control of the temperature of the heat sink is realized by the forced flow...

Claims

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Application Information

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IPC IPC(8): F25D3/10B01L7/00G01M15/14
Inventor 黄永华吴静怡许煜雄李雪元承磊王珊珊
Owner SHANGHAI JIAO TONG UNIV
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