A kind of vanadium dioxide multilayer film system and its preparation method and application

A vanadium dioxide and multi-layer film technology, applied in the field of physics, can solve the problems affecting the phase transition performance of thin-film materials and the large differences in physical properties, and achieve the goal of reducing the probability of defect generation, reducing the number of layers, and simplifying the multi-layer film system structure. Effect
CN109095499BActive Publication Date: 2021-01-15SHENZHEN UNIV

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
SHENZHEN UNIV
Publication Date
2021-01-15

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Abstract

The invention belongs to the field of physics and particularly relates to a vanadium dioxide multilayer membrane system and a preparation method and application thereof. The vanadium dioxide multilayer membrane system comprises a metal thin membrane layer, a gradient refraction index material thin membrane layer and a vanadium dioxide thin membrane layer which are arranged from bottom to top in sequence. A vanadium dioxide material with a gradient refraction index function is used for the vanadium dioxide multilayer membrane system, so that the membrane layer number required in the vanadium dioxide multilayer membrane system is greatly reduced.
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Description

technical field

[0001] The invention belongs to the field of physics, and in particular relates to a vanadium dioxide multilayer film system and a preparation method and application thereof. Background technique

[0002] With the vigorous development of my country's aerospace industry, the number of spacecraft such as various deep space probes, artificial satellites, space laboratories, and space telescopes has increased year by year. Due to the complexity of the internal equipment of the spacecraft, the power consumption and heat flux of the instrument continue to increase, and at the same time, the changes in the space environment faced by the spacecraft are becoming more and more complex. In general, the external temperature of the spacecraft fluctuates in the range of 150°C to 150°C, and in special environments it can reach 100°C to 400°C. Therefore, the importance of research on heat flow control of spacecraft for the development of aerospace technology is self-evident...

Claims

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