A kind of titanium carbide-zirconium carbide high temperature solar energy selective absorption coating and preparation method thereof
An absorption coating, zirconium carbide technology, applied in solar thermal power generation, coating, metal material coating technology and other directions, can solve the problems of metal particle oxidation, diffusion, agglomeration, failure, optical performance degradation, etc., to achieve excellent high temperature stability Performance, easy operation, and the effect of improving the absorption rate
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0021] A titanium carbide-zirconium carbide high-temperature solar selective absorption coating comprises a heat absorber base, an absorber layer and an anti-reflection layer from the bottom layer to the surface in sequence; the heat absorber base is a polished stainless steel sheet or a copper sheet. The absorbing layer material is a composite of titanium carbide and zirconium carbide, which is prepared by double-target co-sputtering, in which titanium carbide is prepared by DC magnetron sputtering, and zirconium carbide is prepared by radio frequency magnetron sputtering; the absorbing layer is composited The thickness of the material is 35 nm, and the atomic percentage of zirconium in the absorbing layer composite is 0.5%. The material of the anti-reflection layer is aluminum oxide, which is prepared by radio frequency magnetron sputtering, with a thickness of 60 nm.
[0022] The preparation method of the above-mentioned titanium carbide-zirconium carbide high temperature s...
Embodiment 2
[0028]A titanium carbide-zirconium carbide high-temperature solar selective absorption coating comprises a heat absorber base, an absorber layer and an anti-reflection layer from the bottom layer to the surface in sequence; the heat absorber base is a polished stainless steel sheet. The absorbing layer material is a composite of titanium carbide and zirconium carbide, which is prepared by double-target co-sputtering, in which titanium carbide is prepared by DC magnetron sputtering, and zirconium carbide is prepared by radio frequency magnetron sputtering; the absorbing layer is composited The thickness of the material is 80 nm, and the atomic percentage of zirconium in the absorbing layer composite is 3%. The material of the anti-reflection layer is aluminum oxide, which is prepared by radio frequency magnetron sputtering, with a thickness of 30 nm.
[0029] The preparation method of the above-mentioned titanium carbide-zirconium carbide high temperature solar energy selective...
Embodiment 3
[0035] A titanium carbide-zirconium carbide high-temperature solar selective absorption coating comprises a heat absorber base, an absorber layer and an anti-reflection layer from the bottom layer to the surface in sequence; the heat absorber base is a polished stainless steel sheet. The absorbing layer material is a composite of titanium carbide and zirconium carbide, which is prepared by double-target co-sputtering, in which titanium carbide is prepared by DC magnetron sputtering, and zirconium carbide is prepared by radio frequency magnetron sputtering; the absorbing layer is composited The thickness of the material is 55 nm, and the atomic percentage of zirconium in the absorbing layer composite is 0.83%. The material of the anti-reflection layer is aluminum oxide, which is prepared by radio frequency magnetron sputtering, with a thickness of 46 nm.
[0036] The preparation method of the above-mentioned titanium carbide-zirconium carbide high temperature solar energy selec...
PUM
| Property | Measurement | Unit |
|---|---|---|
| thickness | aaaaa | aaaaa |
| thickness | aaaaa | aaaaa |
| thickness | aaaaa | aaaaa |
Abstract
Description
Claims
Application Information
Login to View More 

