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Thermal barrier coating material and preparation method thereof

A thermal barrier coating, general technology, applied in the field of laser processing technology and energy materials, can solve the problems of high equipment requirements, long high temperature reaction time, cumbersome steps, etc. Simple process effect

Inactive Publication Date: 2019-09-20
CHONGQING INST OF EAST CHINA NORMAL UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This preparation method is loaded down with trivial details except step, in synthesizing A 2 B 2 o 7 Also can face following problem when type ceramic material: 1. solid-state method synthesizes A 2 B 2 o 7 Type ceramic materials have a high reaction temperature and a long reaction time at high temperature, which requires a great deal of equipment energy consumption; 2. The sol method has a cumbersome process, requires high raw materials and will produce organic pollution; the hydrothermal method requires high equipment, technical difficulty, and safety performance inferior

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  • Thermal barrier coating material and preparation method thereof
  • Thermal barrier coating material and preparation method thereof
  • Thermal barrier coating material and preparation method thereof

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Experimental program
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Effect test

Embodiment 1

[0031] Oxide Gd with rare earth elements Gd and Yb 2 o 3 , Yb 2 o 3 Oxide ZrO with element Zr 2 According to the molar ratio (Gd+Yb): Zr=2:2, wherein the molar ratio of Gd and Yb is 1:4, respectively calculate and weigh three kinds of oxide raw materials of corresponding mass, and carry out high-energy ball milling as raw materials, and the ball milling speed is 400rpm, ball milling time 12h, using acetone as the ball milling medium, fully and evenly mixed to obtain raw material mixture powder, the mixture powder obtained by ball milling was dried and ground in an oven at 75°C, and the ground raw material was granulated and ground to obtain microscopic particle size For smaller, high-density products, the granulation process is as follows: use organic colloidal materials such as PVA as the binder solute, deionized water as the solvent, and configure a binder with a mass fraction of 8%. Add three times to the uniformly mixed powder, grind for 3 hours, sieve, the mesh number...

Embodiment 2

[0033] Oxide Er with rare earth elements Er and Yb 2 o 3, Yb 2 o 3 Oxide ZrO with element Zr 2 According to the molar ratio (Er+Yb): Zr=2:2, wherein the molar ratio of Er and Yb is 1:5, respectively calculate and weigh three kinds of oxide raw materials of corresponding mass, and carry out high-energy ball milling as raw materials for mixing, and the ball milling speed is 400rpm, ball milling time 24h, using ethanol as the ball milling medium, fully and evenly mixed to obtain raw material mixture powder, the mixture powder obtained by ball milling was dried and ground in an oven at 80°C, and the ground raw material was granulated and ground to obtain microscopic particle size For smaller, high-density products, the granulation process is as follows: use organic colloidal materials such as PVA as the binder solute, deionized water as the solvent, and configure a binder with a mass fraction of 6%. Add three times to the uniformly mixed powder, grind for 4 hours, sieve, the m...

Embodiment 3

[0035] Oxide Yb of rare earth element Yb 2 o 3 Oxide ZrO with element Zr 2 According to the molar ratio Yb:Zr=2:2, calculate and weigh two kinds of oxide raw materials of corresponding mass respectively, and weigh high-purity SiO 2 Nanopowder with a mass of 25% of the mass of the first two oxides to prepare SiO 2 / Yb 2 Zr 2 o 7 Composite thermal barrier coating to improve the corrosion resistance and heat insulation performance of the thermal barrier coating. The three oxide raw materials are mixed by high-energy ball milling, using ethanol as the ball milling medium, the ball milling speed is 400rpm, and the time is 24h, and the raw material mixture is fully and uniformly mixed Powder, the mixture powder obtained by ball milling is dried and ground in an oven at 80°C, and the ground raw materials are granulated and ground to obtain a product with a smaller microscopic particle size and high density. The granulation process is as follows: PVA Use organic colloidal materi...

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Abstract

The invention belongs to the technical field of preparation of key coatings of aeroengines, and concretely relates to a preparation method of a thermal barrier coating of a turbine of an aeroengine. Reaction raw material powder of the thermal barrier coating is uniformly mixed with rare earth oxide powder, the mixed powder is pre-placed on alloy or a metal matrix, laser irradiation or sintering is carried out by controlling laser spot size, power, time and other parameters, and laser resonance intensifies rare earth sensitized ions to realize energy transfer. Continuous laser energy supply re-intensifies the intensified ions and causes a multi-step cascade reaction and energy transfer, thereby inducing the mixed raw materials to be subjected to a high-temperature solid phase reaction to grow a thermal barrier coating on the matrix by self-propagating. The method of the invention has the advantages of low laser energy input and rapid reaction. The prepared thermal barrier coating has high adhesion to the matrix, is uniform, has less cracks, and has good thermal shock resistance. Moreover, the preparation method is high in raw material utilization rate, energy-saving and environmentally friendly, and is suitable for large-scale industrial production.

Description

technical field [0001] The invention belongs to the fields of laser processing technology and energy materials, and in particular relates to a thermal barrier coating material and a preparation method thereof. Background technique [0002] Thermal barrier coatings (Thermal Barrier Coatings, TBCs) are a kind of thermal protection that coats high temperature resistant, low thermal conductivity, and corrosion resistant ceramic materials on the surface of workpieces in the form of coatings to reduce the surface temperature of workpieces in high temperature service environments. Technology, currently mainly used in gas engine turbine blades, can significantly improve the working efficiency and thrust of the engine, and at the same time reduce the working temperature of the blade alloy, thereby greatly improving the life and reliability of the engine. It is an indispensable item for advanced aeroengines key technologies. With the rapid development of the aerospace industry, the g...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B35/66C04B35/48C04B35/50C04B35/622
CPCC04B35/48C04B35/50C04B35/62222C04B35/66C04B2235/3418
Inventor 曾和平黄延伟贺嘉杨
Owner CHONGQING INST OF EAST CHINA NORMAL UNIV