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Method for preparing high-performance carbon/carbon composite material with short period and low cost

A carbon composite material and a composite material technology, which is applied in the field of carbon fiber composite material preparation, can solve the problems of long preparation process cycle, high cost, difficulty in preparing large-sized and high-density C/C composite materials, etc., so as to improve the mechanical properties. , the effect of shortening the preparation cycle

Pending Publication Date: 2019-08-23
INST OF METAL RESEARCH - CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

The disadvantage of the isothermal CVI process is that it is difficult to prepare large-size and high-density C / C composites, and the preparation process is long and expensive

Method used

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  • Method for preparing high-performance carbon/carbon composite material with short period and low cost
  • Method for preparing high-performance carbon/carbon composite material with short period and low cost
  • Method for preparing high-performance carbon/carbon composite material with short period and low cost

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preparation example Construction

[0032] (1) Preparation of interface layer

[0033] Using the CVI process, the carbon fiber prefabricated body is placed in an ICVI furnace to prepare the interface layer, and the thickness of the interface layer ranges from 0.3 to 2 μm.

[0034] (2) Preparation of low-density C / C composite materials

[0035] Using the E-CVI process, the carbon fiber prefabricated body containing the interface layer is placed in an E-CVI furnace with a water wall to deposit a pyrolytic carbon matrix to obtain a low-density C / C composite material, and the overall density is controlled at 0.8-1.6g / cm 3 between;

[0036] (3) Preparation of high-performance, high-density C / C composites

[0037] Using the PIC process, the low-density C / C composite material obtained in step 2 is placed in a vacuum pressure vessel, and the resin is introduced into the material matrix obtained in step 2 by using a vacuum environment, and undergoes vacuum-pressure impregnation, low-temperature drying, cross-linking ...

Embodiment 1

[0047] Take 400×100×15mm as an example, the density is 0.5g / cm 3 2D needle felt; Pyrolytic carbon interface layer prepared by ICVI process, temperature 900°C, argon flow rate 0.2m 3 / h, propane 0.15m 3 / h, the deposition time is 5 hours; the low-density C / C composite material is prepared by E-CVI process, the temperature is 700-1000°C, and the flow rate of argon gas is 0.2m 3 / h, propane 0.15m 3 / h, deposition time 20 hours, prepared material density 1.65g / cm 3 ;The PIC process is used to prepare high-performance and high-density C / C composite materials. After 8 cycles of dipping and cracking, after 2 times of 2000°C and 2h high-temperature heat treatment, the specific process parameters of dipping and cracking are: vacuum degree -0.1MPa, impregnation pressure 5MPa , Curing temperature 170°C, carbonization cracking temperature 1000°C, heat preservation 1h, material final density 1.90g / cm 3 , The total material preparation cycle is 350 hours. figure 2 It is the microstru...

Embodiment 2

[0049] Take 400×100×25mm as an example, the density is 0.5g / cm 3 2D needle felt; Pyrolytic carbon interface layer prepared by ICVI process, temperature 900°C, argon flow rate 0.2m 3 / h, propane 0.15m 3 / h, the deposition time is 5 hours; the low-density C / C composite material is prepared by E-CVI process, the temperature is 700-1000°C, and the flow rate of argon gas is 0.2m 3 / h, propane 0.15m 3 / h, deposition time 30 hours, prepared material density 1.55g / cm 3 ;The PIC process is used to prepare high-performance and high-density C / C composite materials. After 8 cycles of impregnation and cracking, after 2 times of 2000℃-2h high-temperature heat treatment, the specific process parameters of impregnation and cracking are: vacuum degree -0.1MPa, impregnation pressure 5MPa , Curing temperature 170°C, carbonization cracking temperature 1000°C, heat preservation 1h, material final density 1.85g / cm 3 , The total material preparation cycle is 400 hours. image 3 It is the mecha...

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Abstract

The invention discloses a method for preparing a high-performance carbon / carbon composite material with short period and low cost, and belongs to the technical field of preparation of carbon fiber composite materials. In the method, a compound process of an electric coupling chemical vapor deposition process (E-CVI) and a liquid phase impregnation-carbonization process (PIC) is used for preparinga high-performance C / C composite material. The density of the prepared high-performance high-density C / C composite material can reach 1.8-1.9 g / cm<3>, and the preparation period is only 400-500 hours.Compared with a traditional isothermal CVI process, the method has the advantages that the preparation period is shortened by 30-50%, and the cost is reduced by about 1 / 2. The intermediate density C / C composite material (1.45-1.65 g / cm<3>) prepared in the invention can meet the requirement of civil markets, the preparation period is only 200-300 hours, and the cost is only 1 / 4-1 / 3 of the preparation cost of an isothermal CVI process.

Description

technical field [0001] The invention relates to the technical field of carbon fiber composite material preparation, in particular to a short-period, low-cost method for preparing high-performance carbon / carbon composite materials. Background technique [0002] As an advanced composite material, carbon / carbon composites (C / C composites) have dual characteristics of structural materials and functional materials. It has a series of excellent properties such as high specific strength, high specific modulus, high temperature resistance, corrosion resistance, fatigue resistance, creep resistance, low density and small expansion coefficient. At present, it has been widely used in aviation and aerospace fields. Such as rocket engine nozzle throat lining, aircraft brake disc, maglev train skid plate, etc. [0003] The main preparation processes of C / C composites include liquid impregnation pyrolysis (PIC process) and chemical vapor infiltration (CVI process). Among them, the liqui...

Claims

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Application Information

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IPC IPC(8): C04B35/83C04B35/622
CPCC04B35/622C04B35/62873C04B35/83C04B2235/48C04B2235/5256C04B2235/608C04B2235/658C04B2235/77
Inventor 汤素芳庞生洋胡成龙王石军李建
Owner INST OF METAL RESEARCH - CHINESE ACAD OF SCI