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High-efficient radiating system applicable to multiple point heat sources in small space

A heat dissipation system and small-space technology, applied in the field of aerospace thermal control, can solve problems such as the inability to solve the heat dissipation requirements of high-power phased array antennas, poor reliability and stability of mechanical pumps, and occupying space resources, so as to save power and temperature The effect of good operation and convenient layout

Inactive Publication Date: 2015-12-02
BEIJING INST OF SPACECRAFT SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] Currently commonly used heat dissipation methods include air cooling and single-phase water cooling. The disadvantage of air cooling is that it occupies limited space resources. At the same time, in the field of aviation and aerospace, this cooling method cannot be used due to the thin air; pump-driven single-phase fluid circuit scheme Limited by the flow rate of the mechanical pump, it is impossible to solve the heat dissipation requirements of the high-power phased array antenna. At the same time, the reliability and stability of the long-term operation of the mechanical pump are poor, and maintenance is often required

Method used

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  • High-efficient radiating system applicable to multiple point heat sources in small space
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  • High-efficient radiating system applicable to multiple point heat sources in small space

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Embodiment Construction

[0016] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0017] as attached figure 1 and 2 As shown, the present invention is used to dissipate heat on the power amplifier module and the power module on the phased array antenna, that is, the point heat source; because the volume of the phased array antenna assembly is small and the power is large, multiple heat sources work at the same time, such as the phased array antenna assembly. The total heat consumption of the power amplifier module and power module of the control array antenna has reached 1000W.

[0018] The heat dissipation system of the present invention includes a loop heat pipe capillary pump 1, a steam pipeline, a liquid pipeline, a condensation heat exchanger 2, a first flat evaporator 3, a second flat evaporator 4, a third flat evaporator 5, a fourth Flat plate evaporator 6, fifth flat plate evaporator 7 and auxiliary drive heater 8; peripheral ...

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Abstract

The invention discloses a high-efficient radiating system applicable to multiple point heat sources in a small space, belonging to the technical field of aerospace thermal control. The system comprises a loop heat pipe capillary pump, a steam pipeline, a liquid pipeline, a condensation heat exchanger and flat evaporators, wherein the loop heat pipe capillary pump is heated by utilizing the heat of an active heater; a working medium in the loop heat pipe capillary pump is evaporated, and is transferred to the condensation heat exchanger for condensation through the steam pipeline; condensed liquid returns to the flat evaporators through the liquid pipeline, and is evaporated again after absorbing the heat of the point heat sources in the small space; the working medium returns to the condensation heat exchanger for condensation again; the working medium flows back to the loop heat pipe capillary pump after condensation to finish one time of cooling circulation; one or more cooling loops each consisting of the flat evaporators, the steam pipeline, the condensation heat exchanger and the liquid pipeline are connected in series between the condensation heat exchanger and the loop heat pipe capillary pump, so that heat carried by the system can be further increased. By adopting the high-efficient radiating system, high-efficient radiating in the small space can be realized.

Description

technical field [0001] The invention relates to a cooling system, in particular to a high-efficiency cooling system with multiple heat sources in a small space, and belongs to the technical field of aerospace thermal control. Background technique [0002] With the development of electronic technology, the degree of integration of electronic devices is getting higher and higher, and their heat generation is getting larger and larger. With the increase in the number of electronic devices, the installation space is getting smaller and smaller. The problem of heat dissipation of many point heat sources in electronic devices It has become a technical bottleneck restricting its integration and upgrading. [0003] Currently commonly used heat dissipation methods include air cooling and single-phase water cooling. The disadvantage of air cooling is that it occupies limited space resources. At the same time, in the field of aviation and aerospace, this cooling method cannot be used d...

Claims

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Application Information

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IPC IPC(8): F28D15/02H05K7/20
Inventor 丁汀连红奎何江李萌卿恒新张红星李磊苗建印
Owner BEIJING INST OF SPACECRAFT SYST ENG
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