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A kind of manufacturing method of low-cost dual-element carbon matrix aircraft carbon brake disc

A manufacturing method and technology of dual carbon, applied in the direction of brake discs, mechanical equipment, gear transmission mechanisms, etc., can solve the problems that are not conducive to mass industrial production, unstable product quality consistency, poor structure uniformity, etc., to achieve Improve wet braking performance, improve structural uniformity and quality consistency, and reduce the effect of opening ratio

Active Publication Date: 2022-05-10
XIAN CHAOMA SCI TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

First of all, this method uses propylene as the carbon source gas, which has the following disadvantages: (1) the molecular weight of propylene is large, the penetration depth is small, and the carbon deposition efficiency is low; (2) the surface of the preform is easy to form crusts during the densification process, and intermediate Machine processing prolongs the production cycle and increases production costs; (3) The price of propylene is relatively high, and it needs to be transported by tank truck, which increases the transportation cost
Secondly, this method needs to be installed in the inner and outer thermal gradient deposition furnaces respectively according to different types of charcoal discs. The requirements for equipment are relatively high, and the process is complicated, which is not conducive to large-scale industrial production. The consistency is unstable and the uniformity of the structure is poor

Method used

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  • A kind of manufacturing method of low-cost dual-element carbon matrix aircraft carbon brake disc
  • A kind of manufacturing method of low-cost dual-element carbon matrix aircraft carbon brake disc
  • A kind of manufacturing method of low-cost dual-element carbon matrix aircraft carbon brake disc

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0036] This embodiment includes the following steps:

[0037] Step 1. Set the density to 0.50g / cm 3 The needle-punched non-weft carbon cloth integral carbon disc preform is loaded into a high-temperature heat treatment furnace, and subjected to high-temperature pretreatment at a temperature of 1800 ° C; the needle-punched non-weft carbon cloth integral carbon disc preform is composed of carbon fiber plain cloth and carbon The fiber mesh tires are alternately layered and made by radial needle punching;

[0038] Step 2, the needle-punched non-weft carbon cloth integral carbon disc preform after high temperature pretreatment in step 1 is loaded into a vapor deposition furnace with a diameter of 600 mm, and the furnace loading structure is as follows: figure 1 As shown, the needle-punched non-weft carbon cloth integral carbon disc preform 4 after high temperature pretreatment is loaded into the furnace chamber surrounded by the heating element 2 of the vapor deposition furnace to...

Embodiment 2

[0043] This embodiment includes the following steps:

[0044] Step 1. Set the density to 0.70g / cm 3 The needle-punched non-weft carbon cloth integral carbon disc preform is loaded into a high-temperature heat treatment furnace and subjected to high-temperature pretreatment at a temperature of 2400 ° C; the needle-punched non-weft carbon cloth integral carbon disc preform is composed of carbon fiber twill cloth and carbon fiber The mesh tires are alternately layered and made by radial needle punching;

[0045] Step 2: Put the needle-punched non-weft carbon cloth integral carbon disc preform after high temperature pretreatment in step 1 into a vapor deposition furnace with a diameter of 650 mm, and put the needle-punched non-weft carbon cloth as a whole after high temperature pretreatment. The carbon disc preform 4 is loaded into the furnace chamber surrounded by the heating element 2 of the vapor deposition furnace to form a single material column. The top of the single materi...

Embodiment 3

[0050] This embodiment includes the following steps:

[0051] Step 1. Set the density to 0.65g / cm 3 The needle-punched non-weft carbon cloth integral carbon disc preform is loaded into a high-temperature heat treatment furnace, and subjected to high-temperature pretreatment at a temperature of 2000 ° C; the needle-punched non-weft carbon cloth integral carbon disc preform is composed of carbon fiber plain cloth and carbon The fiber mesh tires are alternately layered and made by radial needle punching;

[0052] Step 2: Load the needle-punched non-weft carbon cloth integral carbon disc preform after high temperature pretreatment in step 1 into a vapor deposition furnace with a diameter of φ of 1400 mm. The furnace loading structure is as follows: figure 2 and image 3 As shown, the needle-punched non-weft carbon cloth integral carbon disc preform 4 after high temperature pretreatment is loaded into the furnace chamber surrounded by the heating element 2 of the vapor depositio...

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Abstract

The invention discloses a method for manufacturing an aircraft carbon brake disc with a low-cost dual-element carbon matrix. The method comprises the following steps: 1. performing high-temperature pretreatment on the prefabricated body of the integral carbon disc of needle-punched non-weft carbon cloth; The pretreated needle-punched non-weft carbon cloth integral carbon plate preform is subjected to isothermal vapor deposition to obtain a pyrolytic carbon matrix with a rough layer structure; 3. The pyrolytic carbon matrix is ​​subjected to resin impregnation-carbonization densification to obtain resin-containing carbon The binary carbon matrix; 4. The binary carbon matrix is ​​subjected to high-temperature graphitization treatment to obtain the dual carbon matrix aircraft carbon brake disc. The present invention uses natural gas as the main carbon source gas for isothermal vapor deposition, and utilizes the characteristics of small natural gas molecules, large penetration depth and high gas utilization rate to increase the speed of vapor deposition, shorten the production cycle, and reduce the cost of raw materials and transportation. The structure uniformity and quality consistency of the dual carbon matrix aircraft carbon brake disc are improved, and the invention is suitable for mass industrial production.

Description

technical field [0001] The invention belongs to the technical field of preparation of aircraft carbon brake discs, and in particular relates to a manufacturing method of a low-cost dual-element carbon matrix aircraft carbon brake disc. Background technique [0002] With the development of carbon / carbon composite materials, theoretical innovation, preparation technology and application expansion have been further studied, and the preparation technology of materials has been continuously improved. Quantification will become the future development trend. [0003] At present, there are mainly three types of carbon matrix materials for manufacturing aircraft carbon brake discs at home and abroad: pyrolytic carbon, resin carbon and pitch carbon. The aircraft carbon brake discs produced by major foreign carbon disc manufacturers such as Dunlop in the UK, Carbon Industie in France, and B.F. Goodrich in the United States are all made of a single pyrolysis carbon matrix obtained by c...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B35/83C04B35/622F16D65/12
CPCC04B35/83C04B35/622F16D65/12F16D2200/0082F16D2200/0034C04B2235/614C04B2235/5248
Inventor 李睿赵大明程皓薛宁娟侯卫权苏君明李俏张稳
Owner XIAN CHAOMA SCI TECH