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A kind of multi-material column CVI furnace and aircraft brake disc manufacturing method

A material column and stockpiling technology, which is applied in the field of multi-material column CVI furnace and aircraft brake disc manufacturing, can solve the problems of large loading capacity, increased equipment maintenance pressure, and blockage of exhaust pipe inlet, and achieve the effect of reducing residence time

Active Publication Date: 2022-07-08
CENT SOUTH UNIV
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Chemical vapor infiltration (CVI) is one of the commonly used methods for manufacturing carbon-carbon composite materials for aircraft brake discs at home and abroad. In order to reduce production costs, the equipment used by aircraft brake disc manufacturers has gradually changed from single-material column CVI furnaces to multi-material The transformation of the column type CVI furnace, the loading capacity of the multi-material column type CVI furnace is large, and the required carbon source gas flow rate also increases accordingly. After the carbon source gas supply becomes larger, the deposition tail gas increases, and the tail gas diffuses and deposits in the free space in the furnace , it is easy to cause the inlet of the exhaust pipe to be blocked and increase the pressure of equipment maintenance

Method used

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  • A kind of multi-material column CVI furnace and aircraft brake disc manufacturing method
  • A kind of multi-material column CVI furnace and aircraft brake disc manufacturing method
  • A kind of multi-material column CVI furnace and aircraft brake disc manufacturing method

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Embodiment Construction

[0021] For ease of understanding, the present invention will be further described below with reference to the accompanying drawings.

[0022] see Figure 1 to Figure 3 , figure 1 It is a schematic diagram of the multi-material column CVI furnace provided by the embodiment of the present invention after the furnace body 6 is omitted, figure 2 Yes figure 1 Schematic cross-section of , image 3 It is the multi-material column CVI furnace edge provided by the embodiment of the present invention. figure 2 Sectional view of section line A-A. It should be noted that the purpose of drawing the material column 3 in the figure is to show the working principle of the multi-material column CVI furnace, and the material column 3 is formed by stacking workpieces (such as aircraft brake disc preforms).

[0023] In the furnace body 6 of the multi-column CVI furnace, the stacking table 2 is arranged on the support base 1, and the stacking table 2 is provided with a plurality of stacking...

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Abstract

The invention provides a multi-material column CVI furnace and a manufacturing method for an aircraft brake disc. The multi-material column CVI furnace is used in the carbon-carbon composite material forming process of the aircraft brake disc manufacturing method. A stacking table (2) and a blocking body (5) are arranged in the furnace body of the CVI furnace. A plurality of stacking stations are arranged on the stacking table. The workpieces are stacked at each stacking station to form a material column. All the material columns on the table form the material column group. The baffle is located between the outer contour of the material column group and the inner wall of the furnace body, and surrounds the material column group along the circumference of the furnace body, and its height is not lower than the material column group. There is an air flow channel between the body and the outer contour of the material column group. The multi-material column CVI furnace provided by the present invention is less prone to blockage of the inlet of the exhaust gas pipeline, thereby helping to reduce maintenance costs.

Description

technical field [0001] The invention relates to the field of aircraft brake disc manufacturing, in particular to a multi-material column CVI furnace and a manufacturing method of an aircraft brake disc. Background technique [0002] Chemical vapor infiltration (CVI) is one of the common methods for manufacturing carbon-carbon composite materials for aircraft brake discs at home and abroad. In order to reduce production costs, the equipment used by aircraft brake disc manufacturers has gradually changed from single-material column CVI furnace to multi-material. The column type CVI furnace is transformed. The multi-material column type CVI furnace has a large loading capacity, and the required carbon source gas flow also increases. After the carbon source gas supply increases, the deposition tail gas increases, and the tail gas diffuses and deposits in the free space in the furnace. , it is easy to cause the blockage of the exhaust pipe inlet and increase the maintenance press...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B35/52C04B35/83F27D17/00F27D21/00
CPCC04B35/83C04B35/52F27D17/002F27D21/00C04B2235/656C04B2235/658
Inventor 熊翔张红波王雅雷
Owner CENT SOUTH UNIV
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