In-situ growth SiC nanowire reinforced SiC ceramic matrix composite material and preparation method thereof

A technology for in-situ growth and composite materials, which is applied in the field of in-situ growth of SiC nanowires reinforced SiC ceramic matrix composites and their preparation, can solve the problems of uneven growth, insufficient length, and interference of SiC nanowire growth, and is conducive to densification. The effect of improving the mechanical properties, broadening the application field and improving the mechanical properties

Inactive Publication Date: 2018-04-13
SUZHOU HONGJIU AVIATION THERMAL MATERIALS TECH CO LTD
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AI Technical Summary

Problems solved by technology

However, in this method, the fiber preform is directly immersed in the slurry prepared by mixing polycarbosilane, catalyst, and solvent, and then pyrolyzed to grow SiC nanowires in situ. Gas is generated due to the decomposition of polycarbosilane during the pyrolysis process, and Volume shrinkage occurs by itself, which will interfere with the growth of SiC nanowires, resulting in uneven growth and insufficient length to effectively strengthen the composite material

Method used

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Embodiment Construction

[0016] An in-situ grown SiC nanowire reinforced SiC ceramic matrix composite material consists of reinforcing fibers, SiC nanowires, an interface layer and a SiC matrix; it is characterized in that the SiC nanowires are grown on the reinforcing fibers in situ, and the interface layer is coated on the reinforcement On the surface of the fiber and the SiC nanowire, the SiC matrix is ​​filled in the gap surrounded by the reinforcing fiber and the SiC nanowire; the reinforcing fiber is a C fiber; the diameter of the SiC nanowire is 100nm, and the length is 1mm; the interface The layer is BN with a thickness of 0.05 μm.

[0017] A method for preparing SiC nanowire-reinforced SiC ceramic matrix composite material in situ, characterized in that it comprises the steps in the following order:

[0018] (1) Mix and ball-mill polycarbosilane, ferrocene, and activated carbon at a mass ratio of 1:0.03:5 to obtain a uniform powder precursor, and put it evenly into a graphite crucible;

[00...

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Abstract

The invention relates to an in-situ growth SiC nanowire reinforced SiC ceramic matrix composite material. The in-situ growth SiC nanowire reinforced SiC ceramic matrix composite material consists of areinforced fiber, SiC nanowires, an interface layer and an SiC matrix, and is characterized in that the SiC nanowires are grown on the reinforced fiber in an in-situ manner; the surface of the reinforced fiber and the surfaces of the SiC nanowires are coated with the interface layer; the SiC matrix is filled in a gap surrounded by the reinforced fiber and the SiC nanowires; the reinforced fiber is C fiber or SiC fiber; the diameters of the SiC nanowires are 50 to 200 nm, and the lengths of the SiC nanowires are 0.5 to 3 mm; the interface layer is PyC or BN, and the thickness of the interfacelayer is 0.02 to 0.1 micron. The in-situ growth SiC nanowire reinforced SiC ceramic matrix composite material effectively solves the problem that the SiC nanowires are relatively difficult to distribute uniformly in a fiber perform, and in addition the advantage of the SiC nanowires for the SiC ceramic matrix composite material is sufficiently developed through the in-situ growth SiC nanowires.

Description

technical field [0001] The invention relates to a ceramic matrix composite material and a preparation method thereof, in particular to an in-situ growth SiC nanowire reinforced SiC ceramic matrix composite material and a preparation method thereof. Background technique [0002] SiC ceramic matrix composites have the characteristics of light structure, high specific strength and high ratio modulus, high temperature resistance, good thermal shock resistance, low thermal expansion coefficient, oxidation resistance and corrosion resistance, etc., and have been widely used in aero-engine hot section structural parts, Rocket engine nozzle, combustion chamber and other aerospace fields. As these high-end fields put forward higher requirements on material performance, for example, the engine requires materials to be more resistant to high temperature and withstand greater airflow, and the nozzle part requires materials to withstand greater pressure. Due to the large increase in ambi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B35/571C04B35/622C04B35/628C04B35/80
CPCC04B35/571C04B35/622C04B35/62865C04B35/806C04B2235/5244C04B2235/5248
Inventor 陈照峰廖家豪
Owner SUZHOU HONGJIU AVIATION THERMAL MATERIALS TECH CO LTD
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