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A kind of surface tough anti-erosion protective coating and its preparation method and application

A protective coating and anti-erosion technology, which is applied in the direction of coating, metal material coating process, vacuum evaporation plating, etc., can solve the problems of inability to achieve anti-erosion effect, and achieve easy large-area uniform deposition and distribution Homogeneous, densely structured effect

Active Publication Date: 2021-05-28
宁波工业技术研究院 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The determinant of small-angle erosion rate is hardness (strong plastic deformation resistance), while the determinant of large-angle erosion rate is toughness (strong resistance to fatigue crack initiation and expansion), but aircraft engine blades are subjected to multi-angle impacts, therefore, Simply increasing the hardness cannot achieve a good anti-erosion effect, and it is necessary to increase the toughness of the coating without losing the hardness

Method used

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  • A kind of surface tough anti-erosion protective coating and its preparation method and application
  • A kind of surface tough anti-erosion protective coating and its preparation method and application
  • A kind of surface tough anti-erosion protective coating and its preparation method and application

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preparation example Construction

[0043] Another aspect of the embodiments of the present invention provides a method for preparing an anti-erosion protective coating, which includes:

[0044] provide a substrate;

[0045]And, using the metal Me target as the target material, and using inert gas and nitrogen as the working gas, the first MeN layer, the MeN spring structure layer and the second MeN layer are sequentially deposited on the substrate by using DC magnetron sputtering technology, Prepare the surface tough and anti-erosion protective coating; wherein, the first MeN layer and the second MeN layer are formed by a plurality of erected MeN nanocrystals closely arranged, and the length direction of the erected nanocrystals is parallel to the The thickness direction of the coating; the MeN spring structure layer is formed by a plurality of small units closely arranged, and each small unit includes a first single layer formed by a plurality of first tilted MeN nanocrystals closely arranged and formed by a p...

Embodiment 1

[0063] In this embodiment, the coating structure is "vertical structure + spring structure + vertical structure", and the preparation method includes the following steps:

[0064] (1) The cemented carbide substrate was ultrasonically cleaned with acetone and ethanol for 15 minutes, dried and placed in a vacuum chamber, and pre-vacuumized to 2.0×10 -5 Torr; Then, 37 sccm of argon gas was introduced into the chamber, a DC pulse bias voltage of -100V was applied to the substrate, and the surface of the substrate was etched by an ion beam for 30 minutes;

[0065] (2) Make the surface of the substrate perpendicular to the target, argon and nitrogen (20sccm:20sccm) are introduced into the cavity, the DC magnetron sputtering source is turned on, the DC magnetron sputtering target current is 3.0A, and the substrate DC pulse bias is -300V, sputtering titanium target, depositing a coating of 775nm on the surface of the substrate to form the first TiN layer;

[0066] (3) Make the deflec...

Embodiment 2

[0071] In this embodiment, the coating structure is "vertical structure + spring structure + vertical structure", and the preparation method includes the following steps:

[0072] (1) The high-speed steel substrate was ultrasonically cleaned with acetone and ethanol for 15 minutes, dried and placed in a vacuum chamber, and pre-vacuumized to 2.0×10 -5 Torr; Then, 37 sccm of argon gas was introduced into the chamber, a DC pulse bias voltage of -100V was applied to the substrate, and the surface of the substrate was etched by an ion beam for 30 minutes;

[0073] (2) Make the surface of the substrate perpendicular to the target, argon and nitrogen (20sccm:20sccm) are introduced into the cavity, the DC magnetron sputtering source is turned on, the DC magnetron sputtering target current is 3.0A, and the substrate DC pulse bias is -300V, sputtering titanium target, depositing a coating of 450nm on the surface of the substrate to form the first TiN layer;

[0074] (3) Make the deflec...

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Abstract

The invention discloses a surface tough anti-erosion protective coating as well as a preparation method and application thereof. The protective coating includes a first MeN layer, a MeN spring structure layer and a second MeN layer stacked in sequence in the thickness direction of the coating; the first MeN layer and the second MeN layer are composed of a plurality of vertical MeN nano The crystals are closely arranged, and the length direction of the vertical nanocrystals is parallel to the thickness direction of the coating; the MeN spring structure layer is formed by a plurality of small units closely arranged, and each small unit includes A plurality of tilted MeN nanocrystals arranged in sequence, wherein Me includes any one of Ti, Cr, and Zr. The protective coating provided by the invention adopts the "vertical layer + spring layer + vertical layer" structure, so that the coating has good comprehensive mechanical properties, and the toughness and erosion resistance of the coating are improved without reducing the hardness.

Description

technical field [0001] The invention belongs to the technical field of surface treatment, and in particular relates to a tough and anti-erosion protective coating on the surface, a preparation method and application thereof. Background technique [0002] The development of aero-engine technology puts forward the requirements of light weight, high temperature, high strength and long life for core materials. When the aircraft is taking off and landing, flying at low altitude, or serving in harsh environments such as deserts, solid particles in the air such as sand and dust will have high-speed impact and friction on the surface of the engine blades under the action of high-speed airflow, affecting the dimensional accuracy and accuracy of the blades. The surface quality will cause erosion damage and loss of the blade, which will affect the performance of the engine and shorten the service life. How to slow down and avoid the erosion and wear of engine blades is an urgent probl...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C23C14/06C23C14/35C23C14/02
CPCC23C14/0036C23C14/022C23C14/0641C23C14/345C23C14/35
Inventor 王丽汪爱英孙丽丽柯培玲帅锦涛
Owner 宁波工业技术研究院