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Preparation method of double-layer silicon-oxygen-carbon composite ceramic coating for porous ceramic heat insulation matrix

A porous layer, tetramethyltetravinylcyclotetrasiloxane technology, applied in the field of preparation of double-layer silicon oxycarbon composite ceramic coatings, can solve the problems of thin thickness, single coating structure, easy cracking, etc. The effect of good transition, good bonding strength, excellent high emission performance

Pending Publication Date: 2021-06-25
TIANJIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Based on this, the present invention provides a method for preparing a double-layer silicon-oxygen-carbon composite ceramic coating for porous ceramic heat-insulating substrates, which is simple and effective, and solves the current problems of single coating structure, easy cracking, and thin thickness. And apply it in the field of thermal protection

Method used

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  • Preparation method of double-layer silicon-oxygen-carbon composite ceramic coating for porous ceramic heat insulation matrix
  • Preparation method of double-layer silicon-oxygen-carbon composite ceramic coating for porous ceramic heat insulation matrix
  • Preparation method of double-layer silicon-oxygen-carbon composite ceramic coating for porous ceramic heat insulation matrix

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0036] 1) Preparation of porous layer polysiloxane PSO precursor slurry: 0.50 g of hydrogen-containing polysiloxane (PHMS), 0.50 g of tetramethyl tetravinylcyclic tetrahydiloxane (D 4 VI) and 1.00 g of dimethylsilicrosiliciloxil (PDMS) were mixed for 30 min to obtain a porous layer polysiloxane (PSO) precursor. 4.00G barium aluminum silicon glass powder (BAS) and 4.00g of silicon (Mosi) 2 As the solid filler, 12.00 g of n-hexane is added to a mixture of polysiloxane (PSO) as a solvent, and the ball milling is added to the ball milling material to obtain a porous layer. Polysiloxane PSO precursor slurry.

[0037] 2) Brushing process of the porous layer: The polysiloxane PSO precursor slurry of the porous layer obtained by step 1) is brushing 3 times on the mullite fiber insulation tile. The porous coating on the fiber insulation wool; the coating is placed at room temperature for 2 h, then in an oven at 60 ° C for 2 h, and pyrolyzes for 2 h under an argon atmosphere in the tube fur...

Embodiment 2

[0043] 1) Preparation of porous layer polysiloxane PSO precursor slurry: 0.50 g of hydrogen-containing polysiloxane (PHMS), 0.50 g of tetramethyl tetravinylcyclic tetrahydiloxane (D 4 VI) and 0.43 g of dimethylsilicrosilicon oil (PDMS) were mixed for 30 min to obtain a porous layer polysiloxane (PSO) precursor. 2.86g barium aluminum silica glass powder (BAS) and 2.86 g of silicon (Mosi 2 As the solid filler, 8.58 g of n-hexane is added to a mixture of silicone (PSO) as a solvent to the solid filler, and the ball milling 2h obtains a ball mill, and 0.02 g of a platinum complex catalyst is added to the ball mill to obtain a porous layer. Polysiloxane PSO precursor slurry.

[0044] 2) Brushing process of the porous layer: The PSO precursor slurry of the porous layer obtained by step 1) is brushed 3 times in the mullite fiber insulation tile, to obtain a mullite fiber insulation tile The porous coating is placed at room temperature at room temperature, then in an oven at 60 ° C for 2 ...

Embodiment 3

[0049] 1) Preparation of porous layer polysiloxane PSO precursor slurry: 0.50 g of hydrogen-containing polysiloxane (PHMS), 0.50 g of tetramethyl tetravinylcyclic tetrahydiloxane (D 4 VI) and 2.33 g of dimethyl silicone (PDMS) were mixed for 30 min to give a porous layer polysiloxane (PSO) precursor. 6.66G barium aluminum silicone glass powder (BAS) and 6.66 g of silicon (Mosi) 2 As the solid filler, 19.95 g of n-hexane is added to a mixture of polysiloxane (PSO) as a solvent to obtain a ball mill, and 0.02 g of a platinum complex catalyst is added to the ball milling material to obtain a porous layer. Polysiloxane PSO precursor slurry.

[0050] 2) Brushing process of the porous layer: The polysiloxane PSO precursor slurry of the porous layer obtained by step 1) is brushing 3 times on the mullite fiber insulation tile. The porous coating on the fiber insulation tile; the coating is placed at room temperature for 2 h, then in an oven at 60 ° C for 2 h, and the argon atmosphere is p...

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Abstract

The invention relates to a preparation method of a double-layer silicon-oxygen-carbon composite ceramic coating for a porous ceramic heat insulation matrix. Hydrogen-containing polysiloxane and tetravinyl cyclotetrasiloxane are used as polymer precursors, molybdenum disilicide is used as an emitting agent, barium-aluminum-silicon glass is used as a binder, and a porous layer and a compact layer are respectively formed by judging whether a coating contains a pore-forming agent dimethyl silicone oil or not and changing the pyrolysis temperature. A double-layer SiOC-BAS-MoSi2 coating containing a porous layer and a compact layer is prepared on a mullite fiber heat insulation tile in a two-time brush coating mode. Through the design of the double-layer coating, the high-emission coating with excellent emission performance and mechanical performance is prepared on the mullite fiber ceramic heat insulation tile. The coating is high in thickness, good thermal protection capacity is achieved, the oxidation resistance of the coating can be improved through the compact surface layer of the coating, good emission performance can be provided through the existence of the high-emission agent molybdenum disilicide in the coating, integration of high-temperature thermal protection and emission performance is achieved, and the high application value is achieved.

Description

Technical field [0001] The present invention relates to the field of aerospace insulation, and more particularly to a method for preparing a bilateral silicone composite ceramic coating for a porous ceramic insulating substrate. Background technique [0002] With the deep exploration of the aviation sector, scientists have also evolved on ultra-high-speed aircraft and their related technological research. When the ultra-high speed aircraft passes through the atmosphere, a large amount of heat is aggregated in the airbeller surface area due to pneumatic heating. These heats are transferred to the inside of the aircraft, which will destroy the internal precision equipment and parts to make the aircraft lose their ability to work, and cause disasters. Therefore, the development and research of thermal protection systems for ultra-high-speed aircraft is an important topic, and even become a bottleneck developed by the aircraft. [0003] Ceramic fiber heatup tiles are widely used in t...

Claims

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Application Information

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IPC IPC(8): C04B41/89
CPCC04B41/009C04B41/52C04B41/89
Inventor 苏冬田正凯祝文霞李晓雷季惠明
Owner TIANJIN UNIV