Passive cooling capillary drainage pipe and method for two-phase fluid loop liquid storer

A passive cooling and fluid circuit technology, which is applied in the field of spacecraft thermal control, can solve the problems of low utilization rate of cooling capacity, reduced system reliability, and high input power consumption, and achieves high utilization rate of cooling capacity, good use value, and improved efficiency. The effect of reliability

Active Publication Date: 2018-07-06
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

The liquid receiver refrigeration of AMS-02 is realized by the semiconductor refrigeration chip, and the heat conduction of the semiconductor cooling surface is installed on the outer surface of the liquid receiver shell, and the cold energy is transferred to the inside of the liquid receiver through the side wall of the liquid receiver. Large power consumption, low cooling efficiency, low utilization rate of cooling capacity, and the need for control circuits to regulate, which makes the structure of the liquid receiver more complex, greatly reducing the reliability of the system, and the semiconductor cooling chip will generate a lot of waste heat at the same time, Still need other cooling capacity

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  • Passive cooling capillary drainage pipe and method for two-phase fluid loop liquid storer
  • Passive cooling capillary drainage pipe and method for two-phase fluid loop liquid storer
  • Passive cooling capillary drainage pipe and method for two-phase fluid loop liquid storer

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Embodiment Construction

[0029] Passive cooling capillary drain tube device used in mechanical pump to drive two-phase fluid circuit accumulator, as attached figure 1 As shown, it consists of four parts: the discharge end of the outer sleeve (including the discharge port), the capillary wall section of the outer sleeve, the central tube, and the blind end of the outer sleeve. Among them, the discharge end of the outer sleeve, the capillary wall section of the outer sleeve and the blind end of the outer sleeve are welded to form the outer sleeve (also known as the drain pipe). The outer sleeve and the central pipe are also welded to form a passive cooling capillary discharge. Tube device. When the device is applied to a liquid reservoir, the discharge end and the outer wall surface of the blind end of the outer tube are respectively sealed and welded to the wall surface of the liquid reservoir, so that the opening at both ends of the central tube and the liquid discharge port are located outside the res...

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Abstract

The invention discloses a passive cooling capillary drainage pipe and method for a two-phase fluid loop liquid storer. The passive cooling capillary drainage pipe penetrates through a liquid storer shell, and communicates with an external fluid loop system; and when liquid to be cooled passes through the liquid storer, the passive cooling capillary drainage pipe is used for cooling. A heat exchange mode is adopted to cool the internal of the liquid storer; a temperature control function is achieved only through adjustment of the heating power consumption, so that the structure of the liquid storer is prominently simplified; and meanwhile, the drainage pipe can be locally located in a colder state always, so that bubbles near the drainage pipe are effectively prevented, and emissions of theliquid storer are guaranteed as liquid-phase working mediums.

Description

Technical field [0001] The invention relates to the technical field of spacecraft thermal control, in particular to a passive cooling capillary drain tube and a method for a two-phase fluid circuit accumulator. Background technique [0002] With the rapid development of aerospace technology, the thermal control requirements of high load, large heat flow density, long-distance heat transfer and high-precision temperature control have become increasingly obvious. The mechanical pump-driven two-phase fluid circuit (referred to as the pump drive fluid circuit) technology has become an active Temperature control technology, which has the advantages of low drive power consumption, long transmission distance, strong heat dissipation capacity, and high temperature control accuracy. It is one of the most powerful means to solve the existing thermal control needs. It is also a research in the field of aerospace thermal control at home and abroad in recent years. Hot spot. [0003] The pump ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F25B43/00
CPCF25B43/006
Inventor 张焕冬赵振明孟庆亮于峰颜吟雪申春梅朱许崔进夏晨晖
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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