Environmental barrier coating used for poly-carbon and ceramic base compound material and preparation method thereof

A composite material and ceramic-based technology, applied in the field of environmental barrier coating and its preparation, can solve the problems that affect the service life and protection effect of environmental barrier coating, holes and cracks, etc., and achieve excellent oxidation resistance and high phase structure stability Sexuality, the effect of wide application prospects

Inactive Publication Date: 2017-05-31
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, even for the surface layer system of rare earth silicate, in the environment of aero-engine, the SiO 2 There is still a large possibility of volatilization, which will lead to changes in the composition of the coating, which will directly lead to holes and cracks in the coating process, which will seriously affect the service life and protective effect of the environmental barrier coating.

Method used

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  • Environmental barrier coating used for poly-carbon and ceramic base compound material and preparation method thereof
  • Environmental barrier coating used for poly-carbon and ceramic base compound material and preparation method thereof

Examples

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Embodiment 1

[0023] like figure 1As shown, the embodiment of the present invention provides an environmental barrier coating for multi-component carbon and ceramic matrix composite materials, which includes a silicon bonding layer 2, a mullite layer 3, and a rare earth silicate in sequence from the base material 1 to the outside. Layer 4 and rare earth zirconate layer 5, wherein, the thickness of the silicon bonding layer 2 is 60 μm, the thickness of the mullite layer 3 is 70 μm, the thickness of the rare earth silicate layer 4 is 120 μm, and the thickness of the rare earth zirconate layer 5 The thickness is 120 μm. The material used for the rare earth silicate layer 4 is ytterbium monosilicate, and the material used for the rare earth zirconate layer 5 is lanthanum zirconate.

[0024] The environmental barrier coating for multi-component carbon and ceramic matrix composite materials provided by the embodiment of the present invention includes a silicon bonding layer 2, a mullite layer 3,...

Embodiment 2

[0052] like figure 1 and figure 2 As shown, the embodiment of the present invention provides a method for preparing an environmental barrier coating for multi-component carbon and ceramic matrix composite materials, comprising: step S1, setting a silicon bonding layer 2 on the surface of the base material 1; step S2, Set mullite layer 3 on the surface of silicon bonding layer 2; step S3, set rare earth silicate layer 4 on the surface of mullite layer 3; Step S4, set rare earth zirconate on the surface of rare earth silicate layer 4 Salt layer 5.

[0053] In the preparation method of the environmental barrier coating for multi-component carbon and ceramic matrix composite materials provided by the embodiment of the present invention, a layer of rare earth zirconate layer is added on the surface of the environmental barrier coating of the traditional rare earth silicate system 5. The rare earth zirconate itself does not contain silicon components, which solves the problem of ...

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Abstract

The invention relates to an environmental barrier coating used for a poly-carbon and ceramic base compound material and a preparation method thereof. The environmental barrier coating includes, successively from a substrate material to exterior, a silicon adhesion layer being 60-70 [mu]m in thickness, a mullite layer being 60-80 [mu]m in thickness, a rare earth silicate layer being 100-120 [mu]m in thickness, and a rare earth zirconate layer being 100-150 [mu]m in thickness. In the environmental barrier coating, the rare earth silicate layer can effectively inhibit an element diffusion reaction between the mullite layer and the rare earth zirconate layer, and the rare earth zirconate layer can significantly reduce volatilization of SiO2, so that a defect of poor high-temperature stability of the rare earth silicate layer is solved. During use, the components of the whole coating is not liable to change, so that service life of the coating under environment of an aero-engine can be greatly prolonged, and protective effect is improved.

Description

technical field [0001] The invention relates to the field of functional coating materials, in particular to an environmental barrier coating for multi-component carbon and ceramic matrix composite materials and a preparation method thereof. Background technique [0002] Compared with superalloys, multi-component carbon and ceramic matrix composites have higher high-temperature stability, can withstand higher turbine inlet temperatures, reduce structural weight, and have broad application prospects in high thrust-to-weight ratio aeroengines. Such as silicon carbide ceramic matrix composites (SiC f / SiC,C f / SiC) has excellent oxidation resistance in a high-temperature dry environment, and a dense oxide protective film can be formed on the surface, which can avoid further erosion of the interior of the material by the oxidative environment, and effectively protect the matrix of multi-element carbon and ceramic matrix composite materials. . However, in the working environmen...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B41/89
CPCC04B41/52C04B41/009C04B41/89C04B41/5096C04B41/5024C04B41/5042C04B35/00
Inventor 罗瑞盈
Owner BEIHANG UNIV
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