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Method for producing carbon/carbon skid of magnetic suspension train

A technology of a maglev train and a manufacturing method, which is applied to brake parts, electric vehicles, vehicle parts, etc., can solve the problems of failure of skid function, low thermal conductivity, low interlaminar shear strength, etc., and achieves improved interlaminar shear. strength, improve wear resistance, improve the effect of interlaminar shear strength and thermal conductivity

Inactive Publication Date: 2009-02-11
XIAN AEROSPACE COMPOSITE MATERIALS INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Its disadvantages are: there is no reinforced carbon fiber in the thickness direction of the skid carbon / carbon, the thermal conductivity is small, the interlayer shear strength is low, and delamination defects are prone to occur during use, resulting in the failure of the skid function

Method used

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  • Method for producing carbon/carbon skid of magnetic suspension train
  • Method for producing carbon/carbon skid of magnetic suspension train

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0024] (1) Acupuncture carbon cloth and carbon fiber composite structure quasi-three-dimensional structure prefabricated body, the thickness of the needle-punched carbon cloth is 2-4mm, and the remaining thickness is needle-punched long carbon fiber, and the needle-punched long carbon fiber and fiber in the prefabricated body The weight percentage of net tire is about 75%: 25%.

[0025] (2) Put the prefabricated body into the negative pressure directional flow gas-phase carbon precipitation furnace, adopt the isothermal CVI densification process, the temperature is 1000°C, the pressure in the furnace is 10KPa, and the carbon source gas (C 3 h 6 ) with a flow rate of 100L / h, after 300 hours of densification treatment, a pyrolytic carbon matrix is ​​formed.

[0026] (3) with the porous carbon / carbon body in the vacuum-pressure impregnation tank, the weight of impregnated furfurone resin is 120kg, and adding the SiC ultrafine powder of 6kg (5% of furfurone resin) by weight perce...

Embodiment 2

[0030] (1) Acupunctured carbon cloth and carbon fiber composite structure quasi-three-dimensional structure prefabricated body, which is made of alternately laminated needled carbon cloth and fiber mesh tires, with a thickness of 6-8mm, and the remaining thickness is needled long carbon fiber and fiber The mesh tires are alternately laminated, and the thickness is 25mm. The weight percentage of the needle-punched long carbon fiber and the fiber mesh tire in the preform is 78%:22%.

[0031] (2) Put the prefabricated body into the negative pressure directional flow gas-phase carbon precipitation furnace, adopt the isothermal CVI compaction process, the temperature is 900-1100 °C, the pressure in the furnace is 5KPa, and the carbon source gas (C 3 h 6 ) with a flow rate of 2000L / h, after 500 hours of densification treatment, a pyrolytic carbon matrix is ​​formed.

[0032] (3) the porous charcoal / charcoal green body is in the vacuum-pressure impregnation tank, the furfurone resin...

Embodiment 3

[0036] (1) Acupunctured carbon cloth and carbon fiber composite structure quasi-three-dimensional structure prefabricated body, which is made of alternately laminated needled carbon cloth and fiber mesh tires, with a thickness of 8-10mm, and the rest is needled long carbon fiber and fiber The mesh tires are alternately laminated, and the thickness is 30mm. The weight percentage of the needle-punched long carbon fiber and the fiber mesh tire in the preform is about 85%:15%.

[0037] (2) Put the prefabricated body into the negative pressure directional flow gas-phase carbon precipitation furnace, adopt the isothermal CVI compaction process, the temperature is 950-1200 °C, the pressure in the furnace is 5KPa, and the carbon source gas (C 3 h 6 ) with a flow rate of 3000L / h, after 300-500 hours of densification treatment, a pyrolytic carbon matrix is ​​formed.

[0038] (3) impregnating 80kg of furfuryl ketone resin with the porous carbon / carbon body in a vacuum-pressure impregnat...

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Abstract

The production of carbon / carbon skid for magnetic suspension train includes needle punching process of preparing quasi-3D prefabricated body of carbon cloth and carbon fiber and isothermal CVI densifying process of the prefabricated body inside negative pressure directional flow vapor carbon depositing furnace to form pyrolytic carbon base body; soaking with furfural acetone resin or phenolic resin with superfine SiC, Al2O3 or ZrO2 powder added inside a vacuum-pressure soaking tank; curing, carbonizing and high temperature processing to form the modified binary carbon base skid material. The present invention has high interlayer shearing strength and heat conducting coefficient, excellent wear resistance and low production cost and is suitable for industrial production.

Description

technical field [0001] The invention relates to a method for manufacturing a carbon / carbon composite material for a maglev train skid. Background technique [0002] Maglev transportation is still a new technology in the world, with a maximum operating speed of 500km / h. The maglev train has no wheels, but several pairs of skids instead. When the train brakes suddenly during operation, or needs to be towed to the repair site due to vehicle failure, the skid supports the train to slide on the track without wearing the track. For this reason, the skid is a key component of the maglev train. At present, the maglev train skids introduced in my country are made of two-dimensional carbon cloth reinforced resin carbon composite materials produced in Germany. Its disadvantages are: there is no reinforced carbon fiber in the thickness direction of skid carbon / carbon, the thermal conductivity is small, the interlayer shear strength is low, and delamination defects are prone to occur ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B35/83F16D69/02F16D65/02B60L13/04B22F7/04
Inventor 苏红邓红兵程文苏君明张晓虎崔红姚冬梅吴大云南登茂闫联生郑金煌赵景鹏
Owner XIAN AEROSPACE COMPOSITE MATERIALS INST