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Method for preparation of ceramic matrix composites by ultrashort pulse laser processing assisted CVI

A technology of ultra-short pulse laser and composite materials, which is applied in the field of ceramics, can solve the problems of slow gas transmission, high equipment requirements, and limited increase in material densification rate, so as to reduce density gradient, improve diffusion environment, and improve toughness Effect

Active Publication Date: 2018-04-13
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In U.S. Patent US5411763, when the thermal gradient CVI method is used to prepare porous structure composite materials, the uniformity of densification can be effectively improved, but the gas transmission is slow, the densification rate of the material is limited, and it is difficult to prepare large-sized and heterogeneous components.
In US Patent 4580524, the FCVI method is used to prepare ceramic matrix composites, which can effectively shorten the densification process and improve the density uniformity. However, the heating of each area in the preform mainly depends on heat conduction, resulting in insufficient densification of the cold surface of the preform.
In the German patent DE4142261, the isothermal pressure gradient CVI process is used to prepare porous structure composite materials, which effectively improves the gas transmission capacity, but there is still the problem of uneven densification
The Journal of Inorganic Materials reported in 2007 that Zeng Xierong and others proposed a microwave heating CVI process. By rationally designing the flow field and selecting a suitable precursor gas for this process, the effective mass transfer efficiency of the precursor gas in the prefabricated body can be effectively improved, thereby accelerating the overall process. The densification rate of the prefabricated body, but the process requires high equipment and is still in the experimental stage

Method used

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  • Method for preparation of ceramic matrix composites by ultrashort pulse laser processing assisted CVI
  • Method for preparation of ceramic matrix composites by ultrashort pulse laser processing assisted CVI
  • Method for preparation of ceramic matrix composites by ultrashort pulse laser processing assisted CVI

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0038] Step 1, preparing two-dimensional laminated carbon cloth preforms in two heats, the specific process is:

[0039] (1) Select T300-1K carbon fiber and weave it into two-dimensional plain weave fabric. After superimposing 23 layers, use 1K carbon fiber to stitch and connect along the thickness direction with a stitching distance of 3mm×3mm, and stitch the laminated layers together to obtain the volume density. 0.70g / cm 31. A carbon fiber prefabricated body with a carbon fiber volume fraction of 40.0%.

[0040] (2) Clamp the carbon fiber preform with a graphite mold, place it in a vacuum furnace at 1800°C for 3 hours of degumming and pretreatment, and then use CVI to deposit the pyrolytic carbon interface layer (PyC) on the obtained fiber preform. The preparation process of the PyC interface phase is as follows: deposition temperature 900°C, atmospheric pressure 0.2KPa, propylene flow rate 30ml / min, Ar flow rate 300ml / min, and natural cooling after deposition for 50-60h. ...

Embodiment 2

[0047] Step 1, preparing two-dimensional laminated carbon cloth preforms in two heats, the specific process is:

[0048] (1) Select T300-1K carbon fiber, weave it into a two-dimensional plain weave, and after superimposing 23 layers, use 1K carbon fiber to stitch and connect along the thickness direction with a stitching distance of 3mm×3mm, and stitch the laminated layers together to obtain the volume density 0.70g / cm 3 1. A carbon fiber prefabricated body with a carbon fiber volume fraction of 40.0%.

[0049] (2) Clamp the carbon fiber preform with a graphite fixture, place it in a vacuum furnace at 1800°C for 3 hours of degumming and pretreatment, and then deposit PyC on the obtained fiber preform by CVI. The preparation process of the PyC interface phase is as follows: deposition temperature 920°C, atmospheric pressure 0.23KPa, propylene flow rate 32ml / min, Ar flow rate 310ml / min, natural cooling after deposition for 50-60h. The above process was repeated 2 times.

[00...

Embodiment 3

[0056] Step 1, preparing two-dimensional laminated carbon cloth preforms in two heats, the specific process is:

[0057] (1) Select T300-1K carbon fiber, weave it into a two-dimensional plain weave, and after superimposing 23 layers, use 1K carbon fiber to stitch and connect along the thickness direction with a stitching distance of 3mm×3mm, and stitch the laminated layers together to obtain the volume density 0.70g / cm 3 1. A carbon fiber prefabricated body with a carbon fiber volume fraction of 40.0%.

[0058] (2) Clamp the carbon fiber preform with a graphite fixture, place it in a vacuum furnace at 1800°C for 3 hours of degumming and pretreatment, and then deposit PyC on the obtained fiber preform by CVI. The preparation process of the PyC interface phase is as follows: deposition temperature 910°C, atmosphere pressure 0.22KPa, propylene flow rate 30ml / min, Ar flow rate 305ml / min, and natural cooling after deposition for 50-60h. The above process was repeated 2 times.

...

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Abstract

The invention relates to a method for preparing a ceramic matrix composite through ultrashort pulse laser processing assisted CVI (chemical vapor infiltration). The method comprises steps as follows: a preformed body is subjected to boundary layer deposition in a graphite furnace; the preformed body is subjected to densification process with a CVI method, and the preformed body is taken out when the relative density of the preformed body reaches 30%-70%; the composite is subjected to super-fine micro-pore processing through ultrashort pulse laser, so that a transmission channel of a gaseous precursor is dredged; circular deposition is performed, and the ceramic matrix composite with high density is acquired. The method has the advantages as follows: (1), a preformed body pore structure in the deposition process is improved, the bottleneck effect of deposition is eliminated, and the uniformity and the density of the composite are improved; (2), the strength of the composite is improved; (3), the deposition time is shortened.

Description

technical field [0001] The invention belongs to the field of CVI preparation of ceramic matrix composite materials, and in particular relates to a method for preparing ceramic matrix composite materials assisted by CVI by ultrashort pulse laser processing. In the traditional chemical vapor infiltration (CVI) process, ultrashort pulse laser is used Micropores are processed to regulate the diffusion channels of gaseous precursors, thereby reducing the density gradient of the composite material, shortening its manufacturing cycle, and improving the compactness, density uniformity and mechanical properties of the ceramic matrix composite material. Background technique [0002] Ceramic matrix composites overcome the Achilles heel of ordinary ceramic materials, which are brittle and poor in reliability, and make them have the characteristics of metal-like fracture behavior, insensitivity to cracks, and no catastrophic damage. At the same time, they have the high temperature resista...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B35/80C04B35/565
CPCC04B35/565C04B2235/74C04B2235/77C04B2235/5248
Inventor 王晶刘永胜张青成来飞张立同
Owner NORTHWESTERN POLYTECHNICAL UNIV
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