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Carbon-carbon/aluminium composite material preparation method

An aluminum composite material and aluminum liquid technology, which is applied in the field of carbon-carbon/aluminum composite material preparation, can solve the problems of difficult preparation of prefabricated parts and difficult control of interface reaction

Inactive Publication Date: 2005-01-26
SHANGHAI JIAO TONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention aims at the two key problems of difficulty in preparing carbon / aluminum composite material prefabricated parts and difficult control of interface reaction, based on the existing carbon-carbon composite material preparation method and carbon / aluminum composite material preparation method, a carbon-aluminum composite material preparation method is proposed. The preparation method of carbon / aluminum composite materials enables it to effectively solve the two problems of prefabricated part preparation and interface reaction control in the preparation process of carbon / aluminum composite materials, which helps to simplify the process and reduce costs, thus providing carbon / aluminum composite materials Lay the foundation for a wide range of applications

Method used

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Examples

Experimental program
Comparison scheme
Effect test

example 1

[0018] Example 1. Preparation of needle felt carbon-carbon / aluminum composites

[0019] First, several layers of integral felts with a thickness of 0.2 to 2 cm are stacked, connected as a whole by needle punching, and the designed fiber volume content is reached, carbonized at 1050°C, and then processed by chemical vapor infiltration to make a needle felt. Carbon-carbon preform; then composited with aluminum using a vacuum pressure infusion process to form a carbon-carbon / aluminum composite. Among them, the carbon fiber volume content is 6%, the pyrolytic carbon volume content is 17%, and the others are aluminum matrix.

[0020] The structure of the needle felt carbon-carbon / aluminum composite material is as follows: the fibers in the plane of the preform are distributed randomly, and the proportions in each direction are roughly equal, so that the properties of the produced material are in-plane isotropic. The carbon fibers in the prefabricated parts are all wrapped in a py...

example 2

[0023] Example 2. Preparation of carbon felt carbon fiber laminate carbon-carbon / aluminum composite material

[0024] First of all, T300 carbon fibers with a design thickness are laid in one direction on the single-layer integral felt, and 2 to 20 layers of integral felts with carbon fibers laid on the surface are stacked to form a sandwich structure of carbon fiber-carbon felt-carbon fiber. After the structure is cross-linked into a whole by needle punching and reaches the designed initial density; carbonization treatment is carried out at 1050°C, and finally carbon fiber carbon felt laminate carbon-based skeleton material is made by chemical vapor infiltration. Then adopt the die casting method, under the pressure of 10MPa, the preheating temperature of the preform is 450°C, the temperature of the aluminum liquid is 800°C, the mold temperature is 300°C, the pressure of the press is 10MPa, and the pressure is maintained for 1 minute. After cooling, carbon felt and carbon fibe...

example 3

[0027] Example 3. Preparation of unidirectional carbon fiber reinforced carbon-carbon / aluminum composite material

[0028] After the T300 carbon fiber is laid in one direction in the graphite mold to the designed volume content, pyrolytic carbon is deposited on the surface of the fiber through chemical vapor infiltration, and the aluminum liquid is infiltrated into the preform by vacuum pressure impregnation process, and the carbon-carbon preform is packed Put it into a steel mold, seal the mold and put it into the heating furnace, the upper furnace body and the lower furnace body are heated up separately, the temperature of the closed tank and the molten aluminum reaches 750°C, and the furnace is vacuumed, when the vacuum degree is 1×10 -6 MPa, lift up the crucible containing the aluminum liquid, immerse the sealed mold mouth with the preform into the aluminum liquid, and then pass nitrogen into the furnace with a pressure of 1×10 6 MPa, under the action of the pressure diffe...

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Abstract

A carbon-carbon / aluminum composite material preparing process for high performance materials is provided. The process is as follows: the forming of the carbon fiber blank: the carbon fiber blank is prepared by using arrangement and needling method; the forming of carbon-carbon precast products: the precast product is prepared by binding fiber using densification technology; the combination of the carbon-carbon precast product and aluminum: the carbon-carbon / aluminum composite material is prepared by using vacuum pressure impregnation method or compression moulding method. The invention solves two problems: the preparation of the precast product and interface reaction control.

Description

technical field [0001] The invention relates to a preparation method of a composite material, in particular to a preparation method of a carbon-carbon / aluminum composite material. It is used in the field of preparation of high-performance materials. Background technique [0002] Generally, the preparation process of carbon / aluminum composite materials includes two steps: 1. Preparation of carbon fiber prefabricated parts; 2. Composite with aluminum to form materials. At present, there are many ways to prepare carbon fiber prefabricated parts, but the use of frames or molds to lay fibers manually is still the main method of making carbon fiber prefabricated parts. Due to the softness of carbon fiber itself, the carbon fiber prefabricated parts made by the current technology mainly rely on external means such as frames and molds to maintain the structure and porosity of the prefabricated part, so it cannot be mechanically processed to change the shape of the prefabricated par...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C22C47/02C22C47/08C22C49/06
Inventor 张国定孙晋良任慕苏刘臻祎
Owner SHANGHAI JIAO TONG UNIV