Cement-free in-situ silicon nitride combined silicon carbide prefabricated member and preparation method thereof

A silicon carbide and silicon nitride technology, which is applied in the field of in-situ silicon nitride combined with silicon carbide preforms and its preparation, can solve the problems of incomplete development of nitride crystals, high temperature requirements, and limited performance improvement, avoiding the need for Low melting point phase, improved thermal strength, flexible molding shape

Inactive Publication Date: 2010-09-08
HENAN UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

(2) Large-tonnage machine press forming requires large production investment, high cost and long cycle
(3) Due to the use of machine pressing, it is impossible to make components with complex structures
(4) Some silicon nitride and silicon carbide materials are directly added to the raw materials. Since silicon carbide and silicon nitride are compounds with extremely strong covalent bonds, they can still maintain high bonding at very high temperatures. Strength, which determines the heat treatment process of materials that add silicon nitride and silicon carbide has high temperature requirements, and the improvement of performance is limited
(5) Some silicon nitride and silicon carbide materials are made by adding metal silicon powder to the raw materials, and the material components are reacted to form silicon carbide at high temperature in high-purity nitrogen. However, due to the machine press forming process, the residual silicon in the product The content is high, and the development of nitride crystals is not complete, resulting in the adverse effect of molten silicon on the strength of the material under high temperature service conditions
The above shortcomings make silicon carbide-based refractory materials unable to be used in parts with complex shapes and demanding performance in high-temperature industries

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0023] 83 parts of silicon carbide, 9 parts of metal silicon powder of 0-0.074mm, 3 parts of hydraulic alumina, 5 parts of silicon dioxide micropowder, the total number of parts is 100 parts, plus 0.006% of sodium tripolyphosphate, plus hexametaphosphoric acid Sodium 0.009% was added into a mortar mixer and stirred for 1 min. Add 4.7% (additional) water after stirring, and stir for 3 minutes after adding water.

[0024] Among them, 20 parts of silicon carbide particles of 3-5mm, 26 parts of silicon carbide particles of 1-3mm, 21 parts of silicon carbide particles of 0.074-1mm, 8 parts of silicon carbide of 0.044mm-0.074mm, and 8 parts of silicon carbide of 0-0.044mm share.

Embodiment 2

[0026] 83 parts of silicon carbide, 4.5 parts of metal silicon powder of 0-0.044mm and 0.044mm-0.074mm, 3 parts of hydraulic alumina, 5 parts of silicon dioxide micropowder, the total number of parts is 100 parts, plus sodium tripolyphosphate 0.006%, add sodium hexametaphosphate 0.009%, add to the mortar mixer and stir for 1min. Add 4.7% (additional) water after stirring, and stir for 3 minutes after adding water.

[0027] Among them, 20 parts of silicon carbide particles of 3-5mm, 26 parts of silicon carbide particles of 1-3mm, 21 parts of silicon carbide particles of 0.074-1mm, 8 parts of silicon carbide of 0.044mm-0.074mm, and 8 parts of silicon carbide of 0-0.044mm share.

Embodiment 3

[0029] 83 parts of silicon carbide, 3 parts of metal silicon powder of 0-0.02mm, 0.02mm-0.044mm and 0.044mm-0.074mm, 3 parts of hydraulic alumina, 5 parts of silicon dioxide micropowder, the total number of parts is 100 parts , add 0.006% sodium tripolyphosphate, add 0.009% sodium hexametaphosphate, add to mortar mixer and stir for 1min. Add 4.7% (additional) water after stirring, and stir for 3 minutes after adding water.

[0030] Among them, 20 parts of silicon carbide particles of 3-5mm, 26 parts of silicon carbide particles of 1-3mm, 21 parts of silicon carbide particles of 0.074-1mm, 8 parts of silicon carbide of 0.044mm-0.074mm, and 8 parts of silicon carbide of 0-0.044mm share.

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Abstract

The invention discloses a cement-free in-situ silicon nitride combined silicon carbide prefabricated member and a preparation method thereof. The cement-free in-situ silicon nitride combined silicon carbide prefabricated member is formed by taking silicon carbide, metallic silicon powder, alumina micro powder, silicon dioxide micro powder and hydraulic alumina as materials and additionally adding dispersing agent, water or silica sol. The prefabricated member is formed by adopting a vibration pouring method, is cured and dried and subjected to high-temperature nitrogen treatment in a high-purity flowing nitrogen gas. The prefabricated member has the advantages of easy construction, low cost, flexible product shape, high hot strength, strong corrosion resistance, high wear resistance and the like and is widely applied to parts strictly requiring the hot-state performance, such as a wind-force pipeline of a cement kiln, a blast-furnace throat, an air port, a delivery pipeline of melt metal, a garbage incinerator and the like.

Description

technical field [0001] The invention relates to a silicon carbide prefabricated part used in the industrial high temperature field, in particular to a cement-free in-situ silicon nitride bonded silicon carbide prefabricated part and a preparation method. Background technique [0002] At present, the materials used in wind pipes of cement kilns, blast furnace throats and tuyeres, molten metal conveying pipes and structural components with complex shapes are mainly corundum-based materials and nitride-bonded silicon carbide-based refractory materials. These materials have the following disadvantages: (1) cement is used as one of the components of the bonding system. Since cement contains calcium salts, in aluminum-silicon refractory materials, calcium compounds will form low melting point phases at high temperatures, which will affect the thermal properties of the materials. (2) Large-tonnage machine press forming requires large production investment, high cost and long cycle...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B35/66
Inventor 王慧芳周宁生张三华胡书禾毕玉保孟庆新于仁红
Owner HENAN UNIV OF SCI & TECH
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