A kind of room temperature curing high temperature resistant anticorrosion coating and preparation method thereof

An anti-corrosion coating, room temperature curing technology, applied in the direction of anti-corrosion coatings, fireproof coatings, coatings, etc., can solve the problems of limited temperature resistance, poor corrosion resistance, poor resistance to cold and heat, etc., to slow down high temperature oxidation corrosion, resistance Good corrosion resistance, good heat and cold resistance

Active Publication Date: 2020-08-07
HUNAN AEROSPACE SANFENG SCI & TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The purpose of the present invention is to overcome the deficiencies of the current high temperature resistant coatings. The present invention provides a room temperature curing high temperature resistant anticorrosion coating and its preparation method, which solves the problem that the current high temperature resistant coatings require high temperature curing, poor corrosion resistance, limited temperature resistance, and cold resistance. The problem of poor thermal variability

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  • A kind of room temperature curing high temperature resistant anticorrosion coating and preparation method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0032] A room temperature curing high temperature resistant anti-corrosion coating, composed of A component and B component:

[0033] Component A: It is made of the following raw materials in parts by mass: 40 parts of methylmethoxysilane oligomer, 5 parts of polycarbosilane, 15 parts of silicate compound, 6 parts of ZPO, 8 parts of copper chrome black, low Melting point blend 7.5 parts, potassium hexatitanate whisker 0.6 parts, dispersant 1.2 parts, fumed silica 0.8 parts, silane coupling agent 1.6 parts, ethylene glycol butyl ether acetate 1.3 parts, xylene 13 parts.

[0034] Component B is isopropyl titanate, and the mass fraction is 1.5% of the methoxysilane oligomer.

Embodiment 2

[0036] A room temperature curing high temperature resistant anti-corrosion coating, composed of A component and B component:

[0037] Component A: made of the following raw materials in parts by mass: 28 parts of methylmethoxysilane oligomer, 12 parts of octylmethoxysilane oligomer, 5.5 parts of polycarbosilane, and 6 parts of silicate compound , 5 parts of ZPO, 5 parts of low melting point blend, 15 parts of aluminum powder, 1.8 parts of alumina whiskers, 1.2 parts of dispersant, 1.2 parts of polyamide wax, 0.3 parts of fumed silica, 1.4 parts of silane coupling agent, 1.6 parts of ethylene glycol butyl ether acetate, 16 parts of xylene.

[0038] Component B is isopropyl titanate, and the mass fraction is 1.5% of the methoxysilane oligomer.

Embodiment 3

[0040] A room temperature curing high temperature resistant anti-corrosion coating, composed of A component and B component:

[0041] Component A: made of the following raw materials in parts by mass: 16.5 parts of methylmethoxysilane oligomer, 16.5 parts of octylmethoxysilane oligomer, 6 parts of polycarbosilane, and 12 parts of silicate compound , 2 parts of barium metaborate, 6 parts of ZPO, 2 parts of aluminum powder, 6 parts of copper chrome black, 11.5 parts of low melting point blend, 3.2 parts of potassium hexatitanate whisker, 1.4 parts of dispersant, 0.5 part of montmorillonite, 0.5 parts of fumed silica, 1.6 parts of silane coupling agent, 1.3 parts of ethylene glycol butyl ether acetate, and 13 parts of xylene.

[0042] Component B is isopropyl titanate, and the mass fraction is 1.5% of the methoxysilane oligomer.

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Abstract

The invention relates to a room temperature-curable high temperature-resistant anticorrosion coating. The coating comprises a component A and a component B. The component A comprises, by mass, 30-50 parts of a main film forming substance, 5-10 parts of an auxiliary film forming substance, 5-20 parts of a silicate compound, 5-15 parts of a high temperature-resistant pigment, 5-15 parts of an antirust filler, 5-15 parts of a low melting point blend, 1-5 parts of a high temperature-resistant whisker reinforcement material, 0.5-1.5 parts of a dispersant, 0.5-2 parts of an anti-settling agent, 1-2parts of a silane coupling agent and 10-20 parts of a solvent; and the component B is a titanate catalyst, and accounts for 0.5-3% of the mass of the main film forming substance. The high temperature-resistant coating has the advantages of excellent temperature resistance, good cold and heat exchange resistance, no cracking, and realization of high hardness and high adhesion after a high temperature; and the high temperature-resistant coating also has the advantages of good high temperature resistance, realization of self-curing at room temperature, high crosslink density, good corrosion resistance, simplification of the construction process, saving of the construction energy consumption, and friendliness to the environment.

Description

technical field [0001] The invention relates to a high temperature resistant anticorrosion coating, which belongs to the field of new chemical materials. Background technique [0002] Generally, metals will produce surface oxidation under high temperature conditions. Oxidation will not only cause metal loss, but also cause changes in elements in the alloy, which will seriously affect the quality of the metal and lead to a decrease in service life. Aiming at the problem of high temperature oxidation of metals, high temperature resistant coating materials are currently used more often. The high temperature resistant coating is easy to construct, low in cost and good in temperature resistance, and has been widely used in modern industry, military and aerospace fields. There are many kinds of high-temperature-resistant coatings, which are divided into organic high-temperature-resistant coatings and inorganic high-temperature-resistant coatings. They are widely used in the surfa...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C09D183/04C09D183/16C09D5/08C09D7/61
CPCC08L2201/08C08L2205/025C08L2205/03C08L2205/035C08L2312/00C09D5/08C09D5/18C09D7/61C09D183/04C08L83/04C08L83/16C08K13/02C08K3/34C08K7/08C08K3/36C08K5/103
Inventor 张光武李著初王团结杨艺聪袁欢欢
Owner HUNAN AEROSPACE SANFENG SCI & TECH CO LTD
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