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A kind of ablation-resistant thermal insulation coating and preparation method thereof

A heat-insulating coating and ablation-resistant technology, used in coatings, fire-retardant coatings, etc.

Active Publication Date: 2021-10-15
AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH
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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 prior art and provide an ablation-resistant heat-insulating coating with high compatibility with base materials, high low-temperature toughness, and uniform high-temperature resistance at high temperatures and its preparation method

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  • A kind of ablation-resistant thermal insulation coating and preparation method thereof

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preparation example Construction

[0041] Further, the present invention also provides a preparation method of an ablation-resistant thermal insulation coating, comprising the following steps:

[0042] Dissolving the organometallic salt in the solvent to form a homogeneous solution;

[0043] Add silicone resin and ceramic precursors into the homogeneous solution, and mix uniformly to form component A;

[0044] Spray or brush, and cure to obtain an ablation-resistant thermal insulation coating.

[0045] Further, steps are also included before spraying or brushing,

[0046] Disperse the filler in the solvent, add the surface modifier, mix uniformly to form component B, and mix component A and component B uniformly to form uniform suspension C.

[0047] In the present invention, the solvent of component A and the solvent of component B are the same or different, but they must be mutually soluble, otherwise the solution will easily cause phase separation after mixing, and a uniform suspension C cannot be formed. ...

Embodiment 1

[0055] This embodiment relates to a new type of ablation-resistant heat-insulating coating, and its preparation method is as follows:

[0056] (1) Dissolve 1g of aluminum isopropoxide and 1.5g of zinc isopropoxide in 20g of n-hexane, then add 30g of phenyltrimethoxysilane and 10g of polycarbosilane, and mix with mechanical stirring until there are no solid particles in the solution , forming component A; 3g silicon hexaboride (SiB 6 ) and 2g of potassium hexatitanate were dispersed in 20g of n-hexane, and 1g of γ-aminopropyltriethoxysilane was added, and mixed by mechanical stirring for 30 minutes to form component B, and component A and component B were mixed uniformly to form a uniform suspension of C.

[0057] (2) Clean the surface of the titanium alloy with acetone to remove oil and surface impurities, and perform sandblasting treatment (50 mesh sand grains, 0.5 MPa) on the surface of the titanium alloy.

[0058] (3) Spray the suspension C on the treated titanium alloy s...

Embodiment 2

[0061] This embodiment relates to a new type of ablation-resistant heat-insulating coating, and its preparation method is as follows:

[0062] (1) Dissolve 1g of aluminum isopropoxide and 1.5g of zinc isopropoxide in 20g of n-hexane, then add 20g of methylphenyl silicone resin and 20g of polysiloxane, and mix with mechanical stirring until there is no solid in the solution Particles, forming component A; 3g of zirconium boride (ZrB 2 ) and 2g of potassium hexatitanate were dispersed in 20g of n-hexane, 1g of γ-(methacryloyloxy)propyltrimethylsilane was added, and mixed by mechanical stirring for 30 minutes to form component B, component A and component Part B was mixed well to form a homogeneous suspension C.

[0063] (2) Clean the surface of the titanium alloy with acetone to remove oil and surface impurities, and perform sandblasting treatment (50 mesh sand grains, 0.5 MPa) on the surface of the titanium alloy.

[0064] (3) Spray the suspension C on the treated titanium al...

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Abstract

The invention proposes an ablation-resistant heat-insulating coating and a preparation method thereof, which include an organic silicon resin, a ceramic precursor and an organic metal salt, and the organic metal salt is hydrolyzed during the polymerization reaction of the organic silicon resin and the ceramic precursor to form a metal complex The metal complex is evenly distributed in the interpenetrating three-dimensional network formed by the polymerization of the silicone resin and the ceramic precursor. The invention adopts organic silicon resin and ceramic precursors to form a three-dimensional network and interweaves each other to form an interpenetrating three-dimensional network, and organic metal salts are evenly dispersed in the interpenetrating three-dimensional network to form an ablation-resistant heat-insulating coating with uniform components. Layer, the performance of the final coating in all directions is uniform, which ensures the anti-ablation and heat insulation effect of the coating, and overcomes the physical mixing of the filler and the coating matrix in the existing coating technology, which is prone to uneven mixing Problems that lead to local deviations in coating properties.

Description

technical field [0001] The invention relates to an ablation-resistant heat-insulating coating and a preparation method thereof, belonging to the technical field of functional materials. Background technique [0002] As the flight speed of the new generation of aircraft is getting faster and the flight distance is getting farther and farther, its thermal protection system needs to deal with the aerodynamic environment characterized by high heat flow, high enthalpy, and high stagnation point pressure. Thermal protection coating is an effective means of protection, which can effectively resist the impact of high-speed heat flow and protect the base cabin of the aircraft. Typical high-temperature resistant thermal protection coatings include silicone coatings, thermal barrier coatings, etc. Silicone coatings are prepared by combining silicone resins with inorganic fillers. Realize long-term protective effect in high temperature environment; while thermal barrier coating belongs...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C09D183/04C09D183/16C09D7/63C09D7/61
CPCC08G77/04C08L2201/08C08L2205/02C08L2205/025C09D4/00C09D5/18C09D183/04C09D7/61C09D7/63C08L83/04C08L83/16C08K5/0091C08K3/24C08K3/38C08K13/02
Inventor 许学伟夏雨李峥许孔力江建英谢永旺王国勇赵英民
Owner AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH