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Carbon fiber thermal insulation rigid tile and preparation method thereof

A technology of carbon fiber and thermal insulation tiles, which is applied in the field of functional composite materials, can solve the problems of insufficient mechanical strength and insufficient temperature resistance of rigid thermal insulation tiles, and achieve the effects of stable overall performance, strong oxidation resistance, and uniform distribution

Active Publication Date: 2019-01-04
AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to overcome the disadvantages of insufficient mechanical strength and insufficient temperature resistance of existing carbon fiber rigid insulation tiles, and adopt different technical solutions to finally provide a carbon fiber with higher temperature resistance, light weight and greater strength The light-weight rigid heat-insulating tile and its preparation method can be used as thermal protection materials for ultra-high-temperature sintering furnaces in an oxygen-free atmosphere, high-temperature equipment in nuclear power plants, and chemical reactors, etc.

Method used

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  • Carbon fiber thermal insulation rigid tile and preparation method thereof
  • Carbon fiber thermal insulation rigid tile and preparation method thereof
  • Carbon fiber thermal insulation rigid tile and preparation method thereof

Examples

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preparation example Construction

[0051] In a second aspect, the present invention provides a method for preparing a carbon fiber rigid thermal insulation tile. Please refer to figure 1 , is a process flow chart for the preparation of carbon fiber rigid insulation tiles according to a preferred embodiment of the present invention. Wherein, the preparation method comprises the steps of:

[0052] (1) obtain the wet billet of chopped carbon fiber by wet forming, obtain the dry billet of carbon fiber after drying;

[0053] (2) After mixing the silicone resin prepolymer, crosslinking agent, catalyst and organic solvent, a silicone resin precursor mixed solution is obtained;

[0054] (3) Use the silicone resin precursor mixture to impregnate the carbon fiber dry body, for example, impregnate the carbon fiber dry body through a vacuum impregnation process, so that the carbon fiber dry body absorbs the silicone resin precursor mixture, and then after room temperature curing, carbonization and high temperature heat t...

Embodiment 1

[0064]① Shorten carbon fibers with a diameter of 10 μm to a length of 2 mm, place the chopped carbon fibers in a kettle filled with acetone, and install a stirring and water-cooled reflux device on the top of the kettle. Turn on the stirring and water-cooling reflux device, heat the acetone to 55°C and reflux for 48 hours, and thoroughly clean off the epoxy resin adhesive attached to the surface of the carbon fiber. Filter the cleaned carbon fibers in the kettle through a filter, and dry them in a fume hood to fully volatilize the acetone.

[0065] ②Mix the chopped carbon fiber after degumming with deionized water according to the mass ratio of 1:150, fully stir and beat in the mixing tank, transfer the slurry to the filter tool, filter out most of the water, and then put the wet The billet is loaded into a shaping mold, the wet billet is pressed to a preset height according to the target density of the material, and dried at 120°C for 24 hours to obtain a carbon fiber dry bil...

Embodiment 2 to 22

[0072] Examples 2 to 22 were performed in the same manner as Example 1 except for the contents shown in Table 1 and Table 2 below. The mechanical strength of the prepared carbon fiber rigid insulation tile was tested, and the results are shown in Table 2.

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Abstract

The invention relates to a carbon fiber thermal insulation rigid tile which comprises short carbon fibers and Si / C / O glass bonding phases, wherein the short carbon fibers form a framework, and the Si / C / O glass bonding phases are used for bonding the short carbon fibers. The invention further provides a preparation method of the carbon fiber thermal insulation rigid tile. The bonding phases among the carbon fibers are prepared by silicon resin, and the Si / C / O glass bonding phases are generated during carbonization-crack to function in bonding the short carbon fiber framework. Moreover, as silica glass films can be generated on surfaces of the Si / C / O glass bonding phases after the Si / C / O glass bonding phases are oxidized in a high-temperature aerobic environment, oxygen atoms are stopped from further oxidizing internal substances, the carbon fiber thermal insulation rigid tile has strong oxidation resistance, the silicon resin cracking in inert atmosphere is high in carbon residue rate,and mechanical strength is higher as compared with that of starch used as a bonder.

Description

[0001] This application is a divisional application with an invention title of "a carbon fiber rigid thermal insulation tile and its preparation method". The filing date of the original application is December 2, 2016, and the application number is 201611100591.5. technical field [0002] The invention relates to the technical field of functional composite materials, in particular to a carbon fiber rigid heat-insulating tile and a preparation method thereof. Background technique [0003] Carbon fiber rigid heat insulation tiles have the advantages of high temperature resistance, light weight and porous, and good heat insulation effect. They can be used directly as ultra-high temperature heat insulation materials, and can also be used as raw materials to prepare lightweight ablative materials or oxidation-resistant carbon-based materials through composite resins. ceramic composites. [0004] The U.S. Atomic Energy Commission discloses a method for preparing a fiber heat insul...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B35/80C04B35/01C04B35/622
CPCC04B32/005C04B35/01C04B35/622C04B35/80C04B2235/9684C04B2235/602C04B2235/483C04B2235/48C04B2235/658C04B2235/6567C04B2235/656C04B14/386
Inventor 鲁胜吴宪张凡郭慧赵英民
Owner AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH