Preparation method of strengthened and toughened CrTiNiSiN nano composite coating
A nano-composite coating, strengthening and toughening technology, applied in the direction of coating, nanotechnology, metal material coating technology, etc., can solve the problems of poor interlayer interface quality and bonding force, interlayer peeling, failure, etc. The effect of interlayer interface quality and bonding force, improving load resistance and ensuring hardness value
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0032] The invention provides a method for preparing a toughened CrTiNiSiN nanocomposite coating, comprising the following steps:
[0033] 1) Carry out mirror polishing and ultrasonic cleaning to the base material;
[0034] Carry out mirror polishing and ultrasonic cleaning on the tungsten carbide sample substrate. The tungsten carbide sample substrate is mirror-polished on a metallographic polishing machine. First use w20 diamond powder and rough polishing canvas for rough polishing, and then use w2.5 diamond powder to match The fine polishing flannelette is used for fine polishing, and after the substrate is cleaned by fine polishing, ultrasonic cleaning is carried out in an alcohol solution for 20 minutes.
[0035] 2) The Ti target and the Cr target with a target material purity of 99.9% are installed on the DC target respectively, and the Si target and the CrNi target with a target material purity of 99.99% are installed on the radio frequency target, and the CrNi target i...
Embodiment 2
[0045] Using the same materials and methods as in Example 1, the difference from Example 1 is that in step 1) mirror polishing and ultrasonic cleaning of the substrate, ultrasonic cleaning was performed for 25 minutes; in step 2), the vacuum of the deposition chamber was pumped to 2.7×10 -3 Pa; Step 3) In the deposition of the transitional Cr layer, the working gas pressure in the deposition chamber is maintained at 0.12Pa, and the preparation temperature is at 200°C; in step 4) in the deposition of the CrN coating, the working gas pressure in the deposition chamber is maintained at 0.12Pa, and the preparation temperature is at 200°C; Step 5) In depositing the CrTiNiSiN coating, the pressure of the working gas in the deposition chamber is maintained at 0.12 Pa, the preparation temperature is at 200° C., and the power of the CrNi target is 800 W.
[0046] The cross-sectional morphology scanning electron microscope picture of the Cr / CrN / CrTiNiSiN multilayer nanocomposite coating...
Embodiment 3
[0050] Using the same materials and methods as in Example 1, the difference from Example 1 is that in step 1) mirror polishing and ultrasonic cleaning of the substrate, ultrasonic cleaning was performed for 30 minutes; in step 2), the vacuum of the deposition chamber was pumped to 3.0×10 -3 Pa; Step 3) In the deposition of the transitional Cr layer, the working gas pressure in the deposition chamber is maintained at 0.15Pa, and the preparation temperature is at 250°C; in step 4) in the deposition of the CrN coating, the working gas pressure in the deposition chamber is maintained at 0.15Pa, and the preparation temperature is at 250°C; Step 5) In depositing the CrTiNiSiN coating, the pressure of the working gas in the deposition chamber is maintained at 0.15 Pa, the preparation temperature is at 250° C., and the power of the CrNi target is 1200 W.
[0051] The Cr / CrN / CrTiNiSiN multilayer nano-composite coating cross-sectional morphology scanning electron microscope picture prep...
PUM
| Property | Measurement | Unit |
|---|---|---|
| Nanohardness | aaaaa | aaaaa |
| Elastic modulus | aaaaa | aaaaa |
| Nanohardness | aaaaa | aaaaa |
Abstract
Description
Claims
Application Information
Login to View More 


