Carbon fiber reinforced nickel-based composite material and producing method thereof

A composite material and carbon fiber technology, which is applied in the field of preparation technology of carbon fiber reinforced nickel-based composite materials, can solve the problems of difficult control of the impregnation temperature of reinforced fibers, high complexity of manufacturing equipment, and unfavorable interface bonding state, etc., to improve the interface bonding state , low cost, low density effect

Inactive Publication Date: 2007-11-07
ZHONGBEI UNIV
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  • Claims
  • Application Information

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Problems solved by technology

Due to the high melting point of nickel (1453°C), there are the following problems in the manufacturing process: (1) The immersion temperature of the reinforcing fiber in the liquid metal nickel is not easy to control
(2) Due to the high preparation temperature, the activity of the fiber and the matrix is ​​enhanced, resulting in an enhanced interaction between the fiber and the matrix, which is not conducive to the formation of a good interface bonding state after compounding, thus affecting the perf

Method used

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  • Carbon fiber reinforced nickel-based composite material and producing method thereof
  • Carbon fiber reinforced nickel-based composite material and producing method thereof
  • Carbon fiber reinforced nickel-based composite material and producing method thereof

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Embodiment Construction

[0057] The carbon fiber used in the present invention is a domestic medium-strength polyacrylonitrile (PAN) carbon fiber with a single filament diameter of (6-8) μm and bundled (1000 / bundle), which can be selected according to the design volume ratio of 30-35%.

[0058] Its tensile strength is 2200MPa, elastic modulus is 200GPa, density is 1.78g / cm 3 , carbon content> 95%.

[0059] The base material is electrolytic nickel, the tensile strength is 317MPa, the alloy element copper is industrial pure copper, and the electrodeposition chemicals used are all chemically pure.

[0060] Process flow chart of the present invention is as shown in Figure 1.

[0061] 1. Carbon fiber pretreatment

[0062] In order to avoid the bonding between single fibers and the abrasion between fibers, the surface of the bundled carbon fibers purchased is coated with adhesive, which needs to be removed before use. First, the carbon fibers are wound on the steel wiring wheel. Then put it into a heatin...

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Abstract

The present invention discloses one kind of carbon fiber reinforced Ni-base composite material and its preparation process, and relates to metal-base composite material. The carbon fiber reinforced Ni-base composite material consists of carbon fiber 30-35 vol%, Cu 6-8 vol %, and Ni 57-64 vol %. The technological process of preparing the composite material includes the steps of: pre-treatment of carbon fiber, electrodepositing Cu, washing, neutralizing, electrodepositing Ni, electrodepositing Ni to form, washing, stoving, cutting, vacuum hot pressing in mold, and cooling in the furnace. The present invention prepares the composite material in a three-step electrodepositing process, and the composite material has high heat strength, high elastic modulus, low density, high smelting point and other advantages, and may be used in the vane of gas-burning turbine engine, etc.

Description

technical field [0001] The present invention relates to metal matrix composites, particularly carbon fiber reinforced nickel matrix composites (C f / Ni) preparation process. Background technique [0002] One of the most promising applications of metal matrix composites is in gas turbine engine blades. Such parts operate at high temperatures and close to the highest stresses that existing alloys can withstand, so they have become an important direction for composite materials research. [0003] Most of the work done on metal matrix composites in recent years is based on the composite system of aluminum and aluminum alloy matrices, because this matrix is ​​easier to manufacture, and the manufacturing and use temperatures are lower, and the matrix can be reduced during the manufacturing process. Degree of reaction with fiber. However, for gas turbine parts that require oxidation resistance, creep resistance, and fatigue resistance at high temperatures, aluminum-based composi...

Claims

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Application Information

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IPC IPC(8): C22C49/08C22C49/14C22C47/04C25D3/38C25D3/12C25D5/54B22F3/02C22C47/02
Inventor 胡保全牛晋川董治中白培康
Owner ZHONGBEI UNIV
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