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An isothermal integrated cooling device suitable for micro-nano satellites

A cooling device and micro-nano-satellite technology, applied in cooling/ventilation/heating transformation, modification through conduction heat transfer, electrical components, etc., can solve the problems of heat flow changes and high heat flux density outside the satellite, and achieve simple operation and easy manufacture , the effect of easy installation

Active Publication Date: 2020-09-18
AEROSPACE DONGFANGHONG SATELLITE
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  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

[0004] The technical problem solved by the present invention is: to overcome the deficiencies of the prior art, to provide an isothermal integrated heat dissipation device suitable for micro-nano satellites, and to solve the problem of high heat consumption, high local heat flux of single machine and high heat flow outside the satellite, which are currently faced by micro-nano satellites. drastic changes

Method used

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  • An isothermal integrated cooling device suitable for micro-nano satellites
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Embodiment Construction

[0023] An isothermal integrated cooling device suitable for micro-nano satellites, such as figure 1 shown. The present invention is composed of a heat dissipation plate 1, an isothermal copper plate 2, an L-shaped external heat pipe 4, and an intermediate partition plate 5.

[0024] The thickness of the cooling plate 1 is between 10 and 25.6 millimeters, and there is a cooling coating on the side outside the star, preferably a glass secondary surface mirror (OSR). The thickness of the isothermal copper plate 2 is 1 millimeter. Coat thermal grease between the mounting surface of the copper plate 2 and the heat dissipation plate 1 . The middle partition 5 is installed on the cooling plate 1, and the surface of the middle partition 5 is sprayed with SR107 white paint except for the equipment installation area. The high heat consumption stand-alone unit 3 is installed on the isothermal copper plate 2, and thermal grease is applied between the installation surfaces. Such as fi...

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Abstract

The invention relates to an isothermal integrated heat dissipation device suitable for micro-nanosatellite, in particular to an isothermal integrated heat dissipation device for realizing isothermal inside the satellite by adopting an external heat pipe and a copper plate with high thermal conductivity. The utility model particularly comprises a heat dissipation plate and an outer cabin plate of the satellite with heat dissipation fins; An isothermal copper plate mounted on the inner surface of the structural plate; L-shaped external heat pipes, the number of which is two; Intermediate partition, inside the satellite. The invention has the following beneficial effects: (1) the heat of the high heat consumption single machine equipment can be rapidly and uniformly diffused to the heat dissipation plate through the isothermal copper plate and then radiated out; (2) isothermal copper plate realizes isothermalization on the radiating plate, and heat pipe conducts heat to the intermediate separator to realize isothermalization of the isothermic copper plate and the intermediate separator; (3) when there is a high heat consumption single machine not working, the heat of other single machines can be conducted, and the active heating is not needed, thus saving the energy on the satellite; (4) The thermal control products used are all passive thermal control products with high reliability and strong process realizability.

Description

technical field [0001] The invention relates to an isothermal integrated heat dissipation device suitable for micro-nano satellites, in particular to an isothermal integrated heat dissipation device that uses an externally attached heat pipe and a copper plate with high thermal conductivity to achieve isothermalization inside the satellite. Background technique [0002] With the rapid development of electronic technology, the single-machine manufacturing of electronic equipment is getting smaller and smaller. Small satellites also benefit from the development of electronic technology, and their quality and volume are getting smaller and smaller. Micro-nano satellites integrate many electronic devices, which can realize the function. The integrated development of micro-nano satellites has brought about the problem of satellite thermal control. Due to the small size of electronic equipment and high heat consumption, and the structural panels of satellites are generally compose...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H05K7/20
CPCH05K7/20336H05K7/20509
Inventor 宁东坡徐志明房红军蔡超凡刘宁
Owner AEROSPACE DONGFANGHONG SATELLITE
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