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A kind of carbon fiber rigid insulation tile and preparation method thereof

A carbon fiber and thermal insulation tile technology, 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: 2019-01-08
AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] 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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  • A kind of carbon fiber rigid insulation tile and preparation method thereof
  • A kind of carbon fiber rigid insulation tile and preparation method thereof
  • A kind of carbon fiber rigid insulation tile and preparation method thereof

Examples

Experimental program
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preparation example Construction

[0050] 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:

[0051] (1) obtain the wet billet of chopped carbon fiber by wet forming, obtain the dry billet of carbon fiber after drying;

[0052] (2) After mixing the silicone resin prepolymer, crosslinking agent, catalyst and organic solvent, a silicone resin precursor mixed solution is obtained;

[0053] (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

[0063] 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.

[0064]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

[0071] 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 rigid thermal insulation tile, which comprises chopped carbon fibers constituting a skeleton, and a Si / C / O glass bonding phase for bonding the chopped carbon fibers. The invention also provides a preparation method of the carbon fiber rigid heat insulation tile. The present invention uses silicone resin to prepare the bonding phase between carbon fibers, and generates a Si / C / O glass bonding phase during carbonization and cracking to play the role of bonding the chopped carbon fiber skeleton, and due to the Si / C / O glass bonding After the phase is oxidized in a high-temperature aerobic environment, a layer of silica glass film will be formed on the surface, thereby preventing the oxygen atoms from further oxidizing the internal substances, so it has strong oxidation resistance, and the residue of the cracking of the silicone resin under an inert atmosphere The carbon rate is high, and the mechanical strength is also higher compared with using starch as a binder.

Description

technical field [0001] 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 [0002] 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. [0003] The U.S. Atomic Energy Commission discloses a method for preparing a fiber heat insulating material in U.S. Patent No. 3,577,344. This patent uses chopped carbon fiber, quartz fiber or aluminum silicate and other oxide ceramic fibers as raw materials, uses soluble starch as binder, and prepares the corresponding fiber insulation material green body ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B32/00C04B14/38
CPCC04B32/005C04B35/01C04B35/622C04B35/80C04B2235/48C04B2235/483C04B2235/602C04B2235/656C04B2235/6567C04B2235/658C04B2235/9684C04B14/386
Inventor 鲁胜吴宪张凡郭慧刘斌赵英民
Owner AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH