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Passively cooled capillary drain tube and method for a two-phase fluid circuit reservoir

A passive cooling and accumulator technology, applied in the field of spacecraft thermal control, can solve the problems of low utilization rate of cooling capacity, reduced system reliability, large input power consumption, etc., and achieves high utilization rate of cooling capacity, good use value, The effect of improving reliability

Active Publication Date: 2020-12-18
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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  • Abstract
  • Description
  • Claims
  • 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

Method used

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  • Passively cooled capillary drain tube and method for a two-phase fluid circuit reservoir
  • Passively cooled capillary drain tube and method for a two-phase fluid circuit reservoir
  • Passively cooled capillary drain tube and method for a two-phase fluid circuit reservoir

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Embodiment Construction

[0029] Passively cooled capillary drain arrangement for mechanical pump driven two-phase fluid circuit reservoirs, as attached figure 1 As shown, it consists of four parts: the drain end of the outer casing (including the liquid outlet), the capillary wall section of the outer casing, the central tube, and the blind end of the outer casing. Among them, the outer casing drain end, the outer casing capillary wall section and the outer casing blind end are welded to form the outer casing (also known as the liquid discharge pipe), and the outer casing and the central tube are also welded to form a passive cooling capillary drainage. Tube device. When the device is applied to the liquid reservoir, the outer walls of the drain end and the blind end of the outer casing are sealed and welded to the wall of the liquid reservoir respectively, so that the openings at both ends of the central tube and the liquid outlet are located outside the liquid reservoir, and the outer casing The ca...

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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 pipe and method for a two-phase fluid circuit liquid storage device. Background technique [0002] With the rapid development of aerospace technology, the thermal control requirements of high load, large heat flux density, long-distance heat transfer and high-precision temperature control are becoming more and more obvious. Temperature control technology, which has the advantages of small driving power consumption, long transmission distance, strong heat dissipation capability, and high temperature control accuracy, is one of the most powerful means to solve the existing thermal control needs, and it is also a research topic in the field of aerospace thermal control at home and abroad in recent years. hotspots. [0003] The pump drive fluid circuit system is mainly composed of a liquid receiver, a mechanical pump, a preheater,...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F25B43/00
CPCF25B43/006
Inventor 赵振明张焕冬孟庆亮于峰杨涛夏晨晖赵宇颜吟雪申春梅朱许崔进
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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