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High-efficiency radiation cold plate for spacing

A cold plate and space technology, which is used in refrigerators, indirect heat exchangers, refrigeration and liquefaction, etc., can solve the problems of not being able to meet the requirements of space radiant refrigeration, constrain the structure and performance of radiant cold plates, and achieve light weight. , Improve the connection strength and thermal conductivity, the effect of high structural strength

Inactive Publication Date: 2011-10-05
NO 510 INST THE FIFTH RES INST OFCHINA AEROSPAE SCI & TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the limitations of spacecraft on the size, volume, and weight of radiative cooling devices also restrict the various structures and performances of radiative cold plates.
At present, many radiation heat exchange equipment of my country's spacecraft cannot better meet the requirements of space radiation cooling under restricted conditions.

Method used

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  • High-efficiency radiation cold plate for spacing

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Embodiment Construction

[0013] Such as figure 1 As shown, the present invention adopts a planar honeycomb structure, which is mainly divided into two parts: a bottom plate 1 and a honeycomb 2 . The bottom plate 1 is made of aluminum alloy, is disc-shaped, and has a thickness of 1.5mm. The honeycomb 2 is an aluminum honeycomb, the shape of the honeycomb hole is a regular hexagon, the height of the honeycomb is consistent with the height of the inner plate of the bottom plate, and it is connected to the inner plate of the bottom plate by vacuum brazing.

[0014] Such as figure 2 As shown, the welding of the bottom plate 1 and the honeycomb 2 of the present invention adopts a vacuum brazing method at 200 ° C, and the pull-off force of the welding part 4 between the aluminum honeycomb and the welded bottom plate is greater than 1.5×10 6 Pa, able to withstand 100 cold and hot shocks from room temperature to liquid nitrogen without cracking or peeling off, and the weight of the welded part 4 shall not e...

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Abstract

The invention relates to a radiation cold plate for space, especially a radiation cold plate adopting radiation heat exchanging technology for aerospace space field, the invention comprises a metal mirror face, a baseboard and an aluminum cellular; characterized in that, the cellular is made of aluminum, the cellular hole is regular polygon-shaped, the height of the cellular is consistent with the height of the baseboard inner tray, and the cellular is connected in the baseboard dish-shaped interior by a braze welding mode; each cellular hole is formed to a black body cavity by jet printing the black coating, the back face of the baseboard is a metal mirror face, a plurality of coatings are made by nickel plating, optical polishing, gold plating and transparent silicon oxide film plating. The invention increases the radiation heat exchanging area, improves the radiation surface emitting rate and heat conductivity coefficient, reduces the heat radiation influence of the outer heat flow to the cold plate, has advantages of high structural strength, light weight and high radiation heat exchanging efficiency, the invention can be used for the infrared detecting radiation cooling device, a spacecraft heat control apparatus and a space environment ground simulator and so on space radiation heat exchanging apparatuses.

Description

technical field [0001] The invention relates to a radiation cold plate for space, belonging to the technical field of space low temperature. Background technique [0002] The universe is a high-vacuum, cool black background of about 3-4K, and the space radiation refrigeration technology is a refrigeration and heat transfer technology developed by utilizing the natural high vacuum, deep low temperature and black heat sink conditions of the universe. Its working principle It is: use high-efficiency radiation cold plate to radiate energy to the deep-cold space of the universe, perform radiation heat exchange, reduce the temperature of the target object, and achieve the purpose of cooling. Radiation refrigeration is a passive refrigeration technology, which has many advantages such as good stability, high reliability and no power consumption. Therefore, in spacecraft thermal control tasks, radiation cooling is used as an important thermal control method, such as radiation coole...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F25B23/00F28D21/00B64G1/50
Inventor 朱恩宝潘雁频朱建炳王小军朱玉博
Owner NO 510 INST THE FIFTH RES INST OFCHINA AEROSPAE SCI & TECH
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