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Spaceflight thermal control system enhanced condensing device based on space dot-matrix foam metal

A foam metal, space lattice technology, applied in steam/steam condensers, lighting and heating equipment, etc., can solve the problems of enhancing heat transfer coefficient, increasing resistance, etc., to increase heat transfer area, reduce flow resistance, and prepare low cost effect

Pending Publication Date: 2022-07-01
SOUTHEAST UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the special structure of through-hole metal foam not only enhances the heat transfer coefficient, but also increases the resistance. Therefore, how to coordinate its flow heat transfer characteristics and resistance characteristics has become a difficult research point.

Method used

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  • Spaceflight thermal control system enhanced condensing device based on space dot-matrix foam metal
  • Spaceflight thermal control system enhanced condensing device based on space dot-matrix foam metal
  • Spaceflight thermal control system enhanced condensing device based on space dot-matrix foam metal

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Embodiment Construction

[0019] In order to deepen the understanding of the present invention, the present invention will be described in further detail below with reference to the accompanying drawings. The embodiments are only used to explain the present invention and do not constitute a limitation on the protection scope of the present invention.

[0020] Figure 1-4 A specific embodiment of an aerospace thermal control system strengthening condensation device based on spatial lattice metal foam is shown, including a shell 1, a condensation heat exchange tube 2, a through-hole foam metal 3, and the condensation heat exchange tube 2 is screwed through. In the shell 1, the through-hole metal foam 3 is filled on the outer wall of the condensation heat exchange tube 2 inside the shell 1. The upper and lower ends of the shell 1 are respectively provided with a refrigerant inlet 11 and a refrigerant outlet 12. Inside the shell 1 Refrigerant is passed through, the lower end and the upper end of the conden...

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Abstract

The invention relates to a spaceflight thermal control system enhanced condensation device based on space dot-matrix foam metal. The spaceflight thermal control system enhanced condensation device comprises a shell, condensation heat exchange pipes and the foam metal. Water circulates in the condensation heat exchange tube, refrigerant circulates outside the condensation heat exchange tube, and the outer wall outside the condensation heat exchange tube is filled with a through hole foam metal structure with high hole density. The foam metal is of a filling structure of a space dot-matrix pyramid foam metal enhanced heat exchange framework. Belongs to the field of spaceflight thermal control system devices, along with rapid increase of the heat flux density of high-performance and high-integration electronic devices in the field of spaceflight systems, a water cooling mode is adopted to replace a traditional air cooling mode, and meanwhile heat exchange is conducted in the mode that high-hole-density foam metal is adopted outside a tube to replace a finned tube. While the heat exchange area is increased by the foam metal, the foam metal filling structure of the space dot-matrix reinforced heat exchange framework can greatly reduce the influence of flow resistance, the heat exchange effect is remarkably improved, and efficient heat dissipation is achieved in a limited space.

Description

technical field [0001] The invention relates to the technical field of aerospace thermal control system devices, in particular to an aerospace thermal control system enhanced condensation device based on space lattice foam metal. Background technique [0002] A reliable and efficient thermal control system is one of the primary prerequisites to ensure the safe operation of manned people. With the rapid development of aerospace vehicle manufacturing technology, the thermal reliability indicators of its on-board electronic and electrical equipment are becoming more and more stringent. The heat transfer capacity and temperature uniformity of the heat-carrying device put forward higher requirements. However, traditional electronic cooling solutions such as natural convection, forced convection, and heat pipe cooling can no longer meet the needs. The traditional air-cooled condensing device has high condensation pressure, large power consumption, and unsatisfactory heat exchange...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F28B1/02F28B9/04F28B9/00
CPCF28B1/02F28B9/04F28B9/00
Inventor 陈振乾常静毅许波施娟
Owner SOUTHEAST UNIV
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