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Method for preparing carbon/carbon composite material by liquid precursor atomization

A technology of carbon composite materials and precursors, applied in the field of composite materials, can solve the problems of waste of electric energy and liquid precursors, difficult to meet the requirements of use, uneven gas concentration, etc., achieve high deposition rate and increase the effect of concentration gradient

Inactive Publication Date: 2011-04-13
XI AN JIAOTONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] (1) Due to the complexity of the process and the violent boiling-gasification of the liquid flooding body, it is difficult to control and calculate the concentration of the reaction gas during the deposition process, so that the accuracy and rigor of the research results are not high, and the prepared The reproducibility of the product and the industrial production of the process are limited
[0006] (2) Due to the complexity of the boiling-gasification of the liquid precursor, the gas concentration in the deposition chamber is not uniform, which leads to the macrostructure of the prepared carbon / carbon composite material being limited by the shape of the heating element, and most of them are relatively regular shape, it is difficult to meet the requirements for special-shaped carbon / carbon composite components
This process is affected by complex chemical reactions, heat transfer, reaction thermodynamics, fluid mechanics, boiling heat transfer, and joint effects, so the relationship between the microstructure and properties of the prepared carbon / carbon composites and the apparent process parameters is difficult to obtain from a theoretical perspective. It is also very difficult to realize and control the process parameters in actual operation
[0008] (4) From the perspective of energy consumption and efficiency, in order to make the liquid precursor form a continuous gaseous film (ie, film boiling) in the preform and crack the reaction to generate deposited carbon, a huge heating power is required to ensure that the inside of the preform Have a high enough temperature and a very long time, which has caused a lot of waste of electrical energy and liquid precursors

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  • Method for preparing carbon/carbon composite material by liquid precursor atomization
  • Method for preparing carbon/carbon composite material by liquid precursor atomization
  • Method for preparing carbon/carbon composite material by liquid precursor atomization

Examples

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Embodiment 1

[0082] Embodiment 1: according to the technical scheme of the present invention, in conjunction with the attached figure 1 , the carbon felt produced by Lanzhou Carbon Factory is used as the prefabricated body, and the carbon felt density is 0.1g / cm 3 , is composed of short fibers in any direction. The specific steps of preparing a hollow cylindrical carbon / carbon composite material by the method of the present invention are as follows:

[0083] (1) Prepare a porous prefabricated body, and cut the 2D carbon fiber into a hollow cylinder with an outer diameter of Φ150mm, an inner diameter of Φ100mm, and a height of 100mm;

[0084] (2) Prepare the graphite heating element and its accessories, process the graphite heating element into a diameter of Φ100mm, and a thickness of 110mm, and prepare heat insulating materials of a certain size and shape to protect the furnace body;

[0085] (3) Put the heat insulating material, graphite heating element, and porous prefabricated body in...

Embodiment 2

[0093] Embodiment 2: according to the technical scheme of the present invention, in conjunction with the attached figure 2 , using PAN-3k 2D carbon fiber as a porous prefabricated body with a density of 0.5g / cm 3 . The concrete steps of adopting the method of the present invention to prepare four block-shaped carbon / carbon composite materials are as follows:

[0094] (1) Prepare the porous prefabricated body, and cut the 2D carbon fiber into four pieces of 100×100×20mm 3 cuboid shape;

[0095] (2) Prepare the graphite heating element and its accessories, and process the graphite heating element into two 120×100×30mm 3 The cuboid shape, at the same time prepare a certain size and shape heat insulation material according to the size of the reaction chamber to protect the furnace body;

[0096] (3) Put the heat insulating material, graphite heating element, and porous prefabricated body into the reactor in order to ensure that one side of the prefabricated body is in close c...

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Abstract

The invention discloses a method for preparing a carbon / carbon composite material by liquid precursor atomization. The method comprises: a multiple-point pressure spraying device is adopted to inject precursors into a reactor and a precast body in a liquefaction spraying way, and liquid phase-atomization-gasification rapid deposition is carried out, thus obtaining the carbon / carbon composite material with the density of 1.6-1.8g / cm<3>.The invention has the advantages that the liquid precursor boiling gasification link is omitted, the energy consumption is reduced, and the controllability of precursor concentration and feeding is realized, the control and regulation of liquid hydrocarbon precursor amount are easier, the utilization factor of liquid hydrocarbon is greatly improved, the effect is obvious in trial-production, and the carbon / carbon composite material with the density reaching up to 1.8g / cm<3> is prepared in 8 hours successfully.

Description

Technical field: [0001] The invention belongs to the field of composite materials, and relates to a rapid preparation method of composite materials, in particular to a method for preparing carbon / carbon composite materials by using liquid precursor atomization as a carbon source. Background technique: [0002] Carbon / carbon composites (C / C, carbon / carbon composites) have been widely used in the leading edge of the wing of the space shuttle, the nose cone, the nozzle of the rocket engine, the throat liner, and the brake disc of the aircraft. The role of structural materials and functional components in the aerospace field is irreplaceable. At present, the latest method of preparing carbon / carbon is chemical liquid-vaporized infiltration (Chemical liquid-vaporized infiltration, CLVI, or known as Film boiling CVI, FBCVI), which is different from the traditional preparation method of carbon / carbon composites. (Chemical vapor infiltration, CVI) has the highest densification rate...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B35/83C04B35/622
Inventor 王继平廖宝莲史忠旗黄斌乔冠军金志浩
Owner XI AN JIAOTONG UNIV
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