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Blade tip cutting coating with boundary particle equal size envelope protruding and preparation method thereof

A technology of equal size and particle size, applied in the direction of coating, metal material coating process, melt spraying, etc., can solve the problems of weak bonding of the blade tip surface and irregular distribution of hard ceramic particles on the boundary.

Active Publication Date: 2021-12-28
XI AN JIAOTONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to overcome the deficiencies of the prior art, the object of the present invention is to provide a blade tip cutting coating with prominent boundary particles of equal size envelope and its preparation method, so as to solve the irregular distribution of hard ceramic particles at the boundary of the blade tip surface and The technical problem of weak combination of blade tip and surface

Method used

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  • Blade tip cutting coating with boundary particle equal size envelope protruding and preparation method thereof
  • Blade tip cutting coating with boundary particle equal size envelope protruding and preparation method thereof
  • Blade tip cutting coating with boundary particle equal size envelope protruding and preparation method thereof

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preparation example Construction

[0037] A method for preparing a blade tip cutting coating with a protruding envelope of equal size of boundary particles, the specific preparation steps are as follows:

[0038] Step S1, coating the bonding alloy layer 2 on the blade tip surface 1 with a clean surface;

[0039] Step S2, fixing the blade tip surface 1 coated with the bonding alloy layer, and then placing the blade tip surface expansion plate, so that the blade tip surface and the end surface of the blade tip surface expansion plate remain flush;

[0040] Step S3, spreading hard ceramic particles 3 on the blade tip surface equipped with the blade tip surface expansion plate to ensure that the blade tip surface 1 is completely covered, and then removing the blade tip surface expansion plate;

[0041] Step S4, use a roller with a step to roll along the blade tip surface 1 for one week, so that the far-end points of more than 50% of the hard ceramic particles 3 in the large particles with a particle diameter exceed...

Embodiment 1

[0050] A blade tip cutting coating with a protruding boundary particle equal size envelope, including a Ni71CrSi bonding alloy layer and a cubic boron nitride ceramic particle layer. The cubic boron nitride particles with an average particle size of 50 μm are bonded to the Ni71CrSi bonding alloy On the blade tip surface of the nickel-based superalloy GH4037, among the hard ceramic particles of equal size enveloped at the boundary of the blade tip surface, there are more than 50% of the distance from the distal point of the large hard ceramic particles to the boundary of the blade tip surface Equal, the distance from the distal point of the large hard ceramic particles to the boundary of the tip surface is 0.1-0.25 times the average particle size of the hard ceramic particles, forming a sharp exposure of the outer edges and corners of the cubic boron nitride particles, combined with the GH4037 tip surface Robust, cutting coating with prominent boundary grains and other dimension...

Embodiment 2

[0058] A blade tip cutting coating with a protruding boundary particle equal size envelope, including a Ti20Zr25Cu10Ni bonding alloy layer and a cubic boron nitride ceramic particle layer. The cubic boron nitride particles with an average particle size of 100 μm are bonded to the On the blade tip surface of the nickel-based superalloy GH4037, among the hard ceramic particles of equal size enveloped at the boundary of the blade tip surface, there are more than 50% of the distance from the distal point of the large hard ceramic particles to the boundary of the blade tip surface Equal, the distance from the distal point of the large hard ceramic particles to the boundary of the tip surface is 0.1-0.25 times the average particle size of the hard ceramic particles, forming a sharp exposure of the outer edges and corners of the cubic boron nitride particles, combined with the GH4037 tip surface Robust, cutting coating with prominent boundary grains and other dimensions. The concrete...

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Abstract

The invention discloses a cutting coating with a protruding envelope of equal size of boundary particles and a preparation method thereof, belonging to the technical field of material surface modification and coating. A blade tip cutting coating with a protruding boundary particle equal-size envelope, including a bonding alloy layer and hard ceramic particles, part of the hard ceramic particles are bonded to the blade tip surface through the bonding alloy layer, and the other part of the hard ceramic particles Equal size is enveloped at the boundary of the blade tip surface and protrudes from the boundary of the blade tip surface, and the hard ceramic particles of equal size enveloped at the boundary of the blade tip surface have more than 50% of large hard ceramic particles The distance from the distal point to the boundary of the blade tip surface is equal, and the distance from the distal point of the large hard ceramic particles to the boundary of the blade tip surface is 0.1-0.25 times the average particle diameter of the hard ceramic particles. The enveloping protruding parts such as the boundary particles of hard ceramic particles not only ensure that the coating can effectively protect the blade tip, but also ensure that the inner wall of the casing after cutting is evenly coated and has a good sealing effect.

Description

technical field [0001] The invention relates to the technical field of material surface modification and coating, in particular to a cutting coating with protruding enveloping boundary particles and a preparation method thereof. Background technique [0002] With the intensification of the energy crisis, improving engine efficiency and reducing fuel consumption have become one of the current research hotspots of aero-engines. In modern aeronautical gas turbine engines, tip clearance has a great influence on compressor and turbine efficiency. Studies have shown that for every 1% increase in blade tip clearance, the efficiency will decrease by about 1.5%; and for every 1% decrease in efficiency, the fuel consumption rate will increase by about 2%. Therefore, reducing the tip clearance is an effective way to improve engine efficiency and reduce fuel consumption. However, the blade tip clearance should not be too small, because too small clearance will cause scraping and wear ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C23C4/134C23C4/137C23C4/18C23C4/06C23C4/08
CPCC23C4/134C23C4/137C23C4/18C23C4/06C23C4/08
Inventor 杨冠军石秋生刘梅军赵梦琪李长久
Owner XI AN JIAOTONG UNIV