Extremely-high-temperature anti-ablation heat conduction composite material and preparation method thereof

A composite material and anti-ablation technology, which is applied in the field of extremely high-temperature anti-ablation thermally conductive composite materials and their preparation, can solve the problems of insufficient high-temperature ablation resistance, low thermal conductivity, low bending strength, etc. Excellent corrosion performance, high thermal conductivity, excellent high temperature oxidation resistance

Active Publication Date: 2021-10-29
AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH
View PDF6 Cites 14 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Chinese patent application CN201811363591.3 discloses a thermally conductive ceramic matrix composite material and its preparation method, but the thermal conductivity of the thermally conductive ceramic matrix composite material in this patent application is the highest in the thermally conductive direction (the direction in which h...

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Extremely-high-temperature anti-ablation heat conduction composite material and preparation method thereof
  • Extremely-high-temperature anti-ablation heat conduction composite material and preparation method thereof
  • Extremely-high-temperature anti-ablation heat conduction composite material and preparation method thereof

Examples

Experimental program
Comparison scheme
Effect test

preparation example Construction

[0033] In a first aspect, the present invention provides a method for preparing an extremely high-temperature ablation-resistant heat-draining composite material, the method comprising the following steps:

[0034](1) High thermal conductivity carbon fiber (such as mesophase pitch-based high thermal conductivity carbon fiber) and polyacrylonitrile-based carbon fiber (PAN-based carbon fiber) are used to weave a high thermal conductivity carbon fiber prefabricated body; Thermally conductive carbon fiber prefabricated body; In the present invention, when adopting high thermally conductive carbon fiber (such as mesophase pitch-based high thermally conductive carbon fiber) and polyacrylonitrile-based carbon fiber (PAN-based carbon fiber) to be mixed and woven into high thermally conductive carbon fiber preformed body, the high thermally conductive The carbon fiber prefabricated body can be woven with high thermal conductivity carbon fiber and polyacrylonitrile-based carbon fiber thr...

Embodiment 1

[0062] A method for preparing an extremely high-temperature ablation-resistant heat-draining composite material, the specific steps of which are:

[0063] ① Weaving of high thermal conductivity carbon fiber prefabricated body: three-way orthogonal structure is adopted, 2K mesophase pitch-based high thermal conductivity carbon fiber is used in the thermal conductivity direction (marked as X direction), and PAN-based T700 is used in the other two directions (Y direction and Z direction) The carbon fiber is mixed and woven, the mesophase pitch-based high thermal conductivity carbon fiber accounts for 82% of the volume fraction of the total carbon fiber in the high thermal conductivity carbon fiber preform, and the volume density of the high thermal conductivity carbon fiber preform is 1.1g / cm 3 .

[0064] ②Preparation of the carbon interface layer: first prepare a pyrolytic carbon interface layer on the fiber surface of the high thermal conductivity carbon fiber prefabricated bod...

Embodiment 2

[0069] Embodiment 2 is basically the same as Embodiment 1, the difference is:

[0070] Embodiment 2 does not comprise step ④, does not carry out HfC-TaSi 2 Preparation of ultra-high temperature ceramic coatings.

[0071] The performance indexes of the materials finally prepared in this embodiment are shown in Table 1.

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

PropertyMeasurementUnit
Thermal conductivityaaaaaaaaaa
Tensile strengthaaaaaaaaaa
Tensile modulusaaaaaaaaaa
Login to view more

Abstract

The invention relates to an extremely-high-temperature anti-ablation heat conduction composite material and a preparation method thereof. The method comprises the following steps of: mixing and weaving high-thermal-conductivity carbon fibers and polyacrylonitrile-based carbon fibers to form a high-thermal-conductivity carbon fiber preform, or weaving high-thermal-conductivity carbon fiber rods to form the high-thermal-conductivity carbon fiber preform; preparing a carbon interface layer on the fiber surface of the high-thermal-conductivity carbon fiber preform by adopting a chemical vapor deposition method and a high-temperature graphitization treatment method in sequence to obtain a heat conduction composite preform; sequentially using a polycarbosilane ceramic precursor and a hafnium tantalum ceramic precursor as impregnation liquid so as to make the heat conduction composite material preform subjected to a PIP process to prepare a heat conduction ultrahigh-temperature ceramic-based composite material; and preparing an anti-ablation ceramic coating on the surface of the heat conduction ultrahigh-temperature ceramic-based composite material to prepare the extremely-high-temperature anti-ablation heat conduction composite material. The extremely-high-temperature anti-ablation heat conduction composite material prepared by the method of the invention has the advantages of high heat conductivity, high density, excellent mechanical properties, excellent high-temperature anti-ablation performance and the like.

Description

technical field [0001] The invention belongs to the technical field of composite material preparation, and in particular relates to an extremely high-temperature anti-ablation heat-draining composite material and a preparation method thereof. Background technique [0002] In spacecraft thermal control systems, thermally conductive materials are widely used in instruments and equipment that require enhanced heat conduction to perform functions such as heat dissipation of devices, uniform temperature of equipment, waste heat transfer, and reduction of contact thermal resistance. Different application requirements put forward different requirements for thermal conductivity, thermal expansion coefficient, high and low temperature resistance, working fluid compatibility, density, mechanical properties and processability of thermal management materials. [0003] High thermal conductivity carbon fiber has great application prospects in various fields due to its ultra-high modulus, ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): C04B35/66C04B35/80C04B35/83C04B35/56C04B35/565C04B41/87
CPCC04B35/66C04B35/80C04B35/83C04B35/565C04B35/5622C04B41/5057C04B41/5071C04B41/87C04B41/009C04B2235/5248C04B2235/3839C04B2235/3891C04B2235/9607
Inventor 张昊张宝鹏刘伟霍鹏飞陈昊然于新民刘俊鹏
Owner AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products