A Method for Fusion Siliconization of Small-sized Circular Section Ceramic Matrix Composite Components

A technology of composite material components and circular cross-sections, applied in furnaces, lighting and heating equipment, crucible furnaces, etc., can solve the problems of uniform density of components, liquid silicon at the bottom of easy deformation, and difference in internal and external density gradients, and achieve low cost and penetration Simple tooling, prevent easy accumulation effect

Active Publication Date: 2022-05-13
XIAN XINGUI CERAMIC COMPOSITE MATERIAL CO LTD
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Problems solved by technology

[0011] In order to solve the problems existing in the LSI process of small-size circular cross-section ceramic matrix composite components, such as easy to produce internal and external density gradient differences, poor component density uniformity, easy deformation, easy accumulation and bonding of liquid silicon at the bottom, etc., the present invention provides a Fused siliconizing method of ceramic matrix composite components with small size and circular cross section

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  • A Method for Fusion Siliconization of Small-sized Circular Section Ceramic Matrix Composite Components
  • A Method for Fusion Siliconization of Small-sized Circular Section Ceramic Matrix Composite Components
  • A Method for Fusion Siliconization of Small-sized Circular Section Ceramic Matrix Composite Components

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Embodiment Construction

[0053]The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0054] The ceramic-matrix composite material member with a small circular cross-section in the present invention generally refers to a ceramic-matrix composite material member whose maximum circular cross-section diameter is less than or equal to 500 mm and whose height is less than or equal to 500 mm.

[0055] In this embodiment, the shape of the small-sized circular cross-section ceramic matrix composite member is as follows figure 1 The tapered nozzle shown has a diameter of 500 mm in the radial section at the large end, a diameter of 200 mm in the radial section at the small end, a height of 450 mm, and a wall thickness of 15 mm.

[0056] against figure 1 The components shown in this embodiment adopt the following process to realize fused siliconization:

[0057] Step 1, preparing fused silicon infiltration tooling;

[0058] Step 1.1. Win...

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Abstract

The invention relates to a method for melting and siliconizing a small-sized circular section ceramic matrix composite component. It solves the problems of easy generation of inner and outer density gradient difference, poor uniform density of components, easy deformation, easy accumulation and bonding of liquid silicon at the bottom, etc. It mainly includes the steps of preparing molten silicon infiltration tooling, processing semi-finished products of small-sized circular section ceramic matrix composite material components, and preparing small-sized circular section ceramic matrix composite material components. Filled with SiC sand grains, and at the same time, the filler powder is filled in the gap between the outer wall of the semi-finished product of the small-sized circular section ceramic matrix composite material component and the inner wall of the first crucible unit, that is, the powder filling area; the inner and outer sides are melted and penetrated to effectively improve the uniformity of modification .

Description

technical field [0001] The invention relates to a method for melting and siliconizing a small-sized circular section ceramic matrix composite material component. Background technique [0002] Ceramic matrix composites have excellent properties such as high temperature resistance, high strength, low density, corrosion resistance and low thermal expansion coefficient, and have become one of the most promising new composite materials for heat-resistant parts and high-strength parts such as aviation and aerospace. During the use of composite materials, the porosity of the material directly determines the various properties of the material, and the key to determining the porosity of the material is the densification technology. The densification processes commonly used in ceramic matrix composites mainly include slurry impregnation-hot pressing sintering method, organic precursor pyrolysis method, chemical vapor infiltration method (CVI method), etc. [0003] Slurry impregnation...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B35/65C04B35/622F27B14/04
CPCC04B35/65C04B35/622F27B14/04C04B2235/616C04B2235/77C04B2235/428C04B2235/3826F27B2014/045
Inventor 王鹏张少博张海昇张晰姜伟光李建章
Owner XIAN XINGUI CERAMIC COMPOSITE MATERIAL CO LTD
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