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A kind of intelligent thermal control device and its preparation method

A thermal controller and intelligent technology, applied in the field of spacecraft thermal control, can solve the problems of loss of intelligent adjustment ability due to temperature changes of spacecraft components, difficulty in meeting spacecraft, and reduction of solar absorption rate, etc., so as to ensure intelligent adjustment ability and control Good effect and wide range of emissivity variation

Active Publication Date: 2020-08-07
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, when the sun is shining, the high solar absorptivity will cause the temperature of the device to rise sharply, thus losing the ability to intelligently adjust the temperature of the spacecraft components. solar absorptivity
However, the emissivity variation of existing intelligent thermal control devices is still relatively small, the solar absorption rate is high, and the complex structure makes the preparation process more difficult, and it is difficult to meet the actual needs of spacecraft thermal control.

Method used

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  • A kind of intelligent thermal control device and its preparation method
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  • A kind of intelligent thermal control device and its preparation method

Examples

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Embodiment 1

[0034] A kind of intelligent thermal control device of the present invention, its structural diagram is as follows figure 1 As shown, it is a four-layer composite structure, and the composite structure is covered on a silicon substrate. The composite structure is a reflective layer 1 (a gold film with a thickness of 300nm), a dielectric layer 2 (a magnesium fluoride film with a thickness of 1000nm) from bottom to top. ), a phase change layer 3 (a vanadium dioxide film with a thickness of 30 nm) and an absorptivity control layer 4 (a nano-polyethylene film doped with magnesium oxide particles with a thickness of 5 μm).

[0035] The preparation method of the intelligent thermal control device of this embodiment includes the following steps:

[0036] (1) adopt electron beam evaporation method to prepare the gold thin film that thickness is 300nm on silicon substrate;

[0037] (2) adopt electron beam evaporation method to prepare the magnesium fluoride thin film that thickness is...

Embodiment 2

[0042] A kind of intelligent thermal control device of the present invention, such as figure 1 As shown, it is a four-layer composite structure, the composite structure is covered on the silicon substrate, and the composite structure from bottom to top is the reflective layer 1 (aluminum film with a thickness of 100nm), the dielectric layer 2 (a zinc sulfide film with a thickness of 680nm), and the corresponding The variable layer 3 (a vanadium dioxide film with a thickness of 60 nm) and the absorption control layer 4 (a fluorocarbon resin film doped with titanium oxide particles with a thickness of 1 μm).

[0043] The preparation method of the intelligent thermal control device of this embodiment includes the following steps:

[0044] (1) Prepare a 100nm aluminum film with a thickness of 100nm on a silicon substrate by magnetron sputtering;

[0045] (2) Prepare a zinc sulfide dielectric layer with a thickness of 680nm on the aluminum film prepared in step (1) by electron bea...

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Abstract

The invention discloses an intelligent thermal control device. The intelligent thermal control device adopts the multi-layer composite structure comprising a reflecting layer, a dielectric layer, a phase change layer and an absorptivity adjusting and controlling layer sequentially from bottom to top; and the multi-layer composite structure is located on a base layer. A preparation method of the intelligent thermal control device includes steps as follows: (1) the reflecting layer is prepared on a base with the physical vapor deposition method; (2) the dielectric layer is prepared on the surface of the reflecting layer with the physical vapor deposition method; (3) the vanadium dioxide thin-film phase change layer is prepared on the surface of the dielectric layer with the magnetron sputtering method; (4) the phase change layer is covered with the absorptivity adjusting and controlling layer, and then the intelligent thermal control device is obtained. The prepared intelligent thermal control device has the large emissivity change range and has the good temperature adjusting and controlling effects, the corresponding high emissivity at the high temperature is higher than 0.8, the area of the thermal control device is reduced favorably, and the function density is increased; and meanwhile, the sunlight absorptivity is lower than 0.3, the intelligent adjusting ability of the device can be guaranteed, and the actual demand for thermal control of a space vehicle can be basically satisfied.

Description

technical field [0001] The invention belongs to the technical field of spacecraft thermal control, and in particular relates to an intelligent thermal control device and a preparation method thereof. Background technique [0002] In the orbital space environment, the main heat exchange method between the interior of the spacecraft and the outer space environment is thermal radiation. Due to the large fluctuation range of external ambient temperature, effective thermal control technology must be adopted in order to keep the temperature inside the spacecraft in a suitable range and ensure the normal operation of various equipment components. At present, the thermal control methods used on spacecraft mainly use complex devices such as thermal control coatings, louvers, and heat pipes. However, these devices have disadvantages such as large volume and weight, high energy consumption, and complex mechanical moving devices, which seriously affect the spacecraft. limited load capa...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C23C14/16C23C14/18C23C14/08C23C14/35C23C14/30C23C14/06G05D23/185C09D123/06C09D127/12C09D7/61
CPCC08K2003/222C08K2003/2241C08K2201/011C09D7/61C09D123/06C09D127/12C23C14/0036C23C14/0629C23C14/0694C23C14/081C23C14/083C23C14/086C23C14/16C23C14/18C23C14/30C23C14/35G05D23/185C08K3/22
Inventor 刘东青彭任富程海峰
Owner NAT UNIV OF DEFENSE TECH
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