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Heat sink temperature control system and method for thermal vacuum test

A technology of temperature control system and temperature control system, which is applied in the field of thermal test, can solve the problems of changing the thermal physical properties of the surface, test errors, etc., and achieve the effects of improving reliability and automatic control level, simplifying the system, and improving temperature control accuracy

Inactive Publication Date: 2012-11-07
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
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Problems solved by technology

Since the heating sheet is pasted on the skin of the satellite, the real state of the surface of the spacecraft is changed, thereby changing the thermophysical properties of the surface, resulting in certain experimental errors

Method used

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  • Heat sink temperature control system and method for thermal vacuum test
  • Heat sink temperature control system and method for thermal vacuum test
  • Heat sink temperature control system and method for thermal vacuum test

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Embodiment Construction

[0029] The following is a specific implementation manner of the content of the present invention, and the content of the present invention will be further clarified through the specific implementation mode below. Of course, the following specific embodiments are described only to illustrate different aspects of the present invention, and should not be construed as limiting the scope of the present invention.

[0030] like figure 1 As shown, the temperature control system of the heat sink used for the thermal vacuum test of the present invention mainly includes a refrigeration system, a brine cooler, a brine heating and temperature control system, a circulating pump, a brine buffer container and a heat sink system, the brine heating and temperature control system includes a brine heating and temperature controller for the main heat sink heating and temperature control and a brine heating and temperature controller for the auxiliary heat sink heating and temperature control, Th...

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Abstract

The invention discloses a heat sink temperature control system for a thermal vacuum test, comprising a refrigerating system, a secondary refrigerant cooler, a secondary refrigerant heating and temperature controlling system, a circulating pump, a secondary refrigerant buffer container and a heat sink system, wherein the secondary refrigerant heating and temperature controlling system comprises a secondary refrigerant heater for heating a main heat sink, a temperature controller for controlling temperature, a secondary refrigerant heater for heating an auxiliary heat sink and a temperature controller for controlling temperature, so that the temperature of a secondary refrigerant entering a heat sink is controlled by the secondary refrigerant heaters and the temperature controllers. The invention also discloses a temperature control method. Compared with the prior art, the heat sink temperature control system can be used for regulating the temperature of the heat sink in a fixed point, and the temperature of a test piece can be regulated and controlled without infrared electric heating equipment, so that the system is simplified, and the temperature control accuracy is improved.

Description

technical field [0001] The invention belongs to the thermal test technical field in space environment simulation, and in particular relates to a temperature control system and a temperature control method of a heat sink used in a thermal vacuum test. Background technique [0002] Thermal vacuum test is a test unique to spacecraft. It verifies the ability of spacecraft components, subsystems and the entire spacecraft to meet the specified requirements under specified vacuum and thermal cycle conditions, thereby exposing the spacecraft in terms of materials, processes and manufacturing. Potential defects in quality, evaluation of operational performance, tests to verify flight performance. In the thermal vacuum test, it is necessary to control the temperature of the components of the spacecraft within the specified range to verify its working performance. Therefore, in addition to providing a vacuum and cool black environment, thermal vacuum test equipment also requires tempe...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D23/19
Inventor 丁文静刘敏张磊刘波涛童华刘然何超李高李昂付春雨
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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