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A kind of silicon carbide ceramic matrix composite material with layered distribution of rare earth silicate and preparation method thereof

A silicon carbide ceramic base and rare earth silicate technology, which is applied in the field of silicon carbide ceramic base composite material with rare earth silicate layered distribution and its preparation, can solve problems such as poor water and oxygen resistance, and achieve excellent mechanical properties, The effect of improving the intrinsic resistance to water and oxygen

Active Publication Date: 2021-07-13
SHANGHAI INST OF CERAMIC CHEM & TECH CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the problem of poor water and oxygen resistance of silicon carbide ceramic matrix composite materials, the object of the present invention is to provide a silicon carbide ceramic matrix composite material with layered distribution of rare earth silicate and its preparation method

Method used

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  • A kind of silicon carbide ceramic matrix composite material with layered distribution of rare earth silicate and preparation method thereof
  • A kind of silicon carbide ceramic matrix composite material with layered distribution of rare earth silicate and preparation method thereof
  • A kind of silicon carbide ceramic matrix composite material with layered distribution of rare earth silicate and preparation method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0058](1) Pretreatment of fiber preform: perform chemical vapor infiltration on the three-dimensional needle-punched carbon fiber preform to prepare a pyrolytic carbon interface layer with a thickness of about 200 nm and a pre-deposited SiC layer with a thickness of 1 μm;

[0059] (2) Preparation of rare earth salt solution: Yttrium nitrate hexahydrate (Y(NO 3 ) 3 ·6H 2 0) powder is dissolved in ethanol, and magnetic stirring obtains the yttrium nitrate / ethanol solution of 1.5mol / L in 24 hours;

[0060] (3) Surface coating and impregnation: soak the preform with the yttrium nitrate / ethanol solution in (2) by surface coating method, and then evaporate to dryness at 90°C for 1 hour to obtain C f / SiC-Y(NO 3 ) 3 ;

[0061] (4) pyrolysis: the C in (3) f / SiC-Y(NO 3 ) 3 Put it into a carbon tube furnace and pyrolyze it in an argon atmosphere, the pyrolysis temperature is 700°C, and keep it warm for 30 minutes to get C f / SiC-Y 2 o 3 ;

[0062] (5) Repeat (3) (4) steps t...

Embodiment 2

[0068] The preparation steps are similar to those in Example 1, except that in step (1), a two-dimensionally stitched silicon carbide fiber preform is used, and a boron nitride interface phase with a thickness of about 200 nm and a preform of 3 μm are prepared on the fiber. A SiC layer is deposited.

[0069] SiC prepared in this embodiment 2 f / SiC-(Y 2 Si 2 o 7 ) 3 The cross-sectional SEM photograph of the composite material is as Figure 4 shown, from Figure 4 As can be seen in the white Y 2 Si 2 o 7 The enrichment area is distributed in multiple layers around the fiber bundle, where Y 2 Si 2 o 7 The thickness of the layer is generally distributed between 200-2000 nm, and the thickness of the SiC layer is 3-5 μm. The composite material prepared in the present embodiment 2 is subjected to a water-oxygen corrosion test, the corrosion temperature is 1400°C, and the atmosphere is 500ml / min (200ml O 2 +300ml H 2 O). After 70 hours of corrosion, the mass loss was -...

Embodiment 3

[0071] The preparation steps are similar to those in Example 1, except that in step (8), steps (3) to (7) are repeated once to fill the SiC matrix. The C prepared in this embodiment 3 f / SiC-(Y 2 Si 2 o 7 ) 2 The composite material was subjected to the water-oxygen corrosion test, the corrosion temperature was 1400°C, the atmosphere was 500ml / min (200ml O 2 +300ml H 2 O). After 70 hours of corrosion, the mass loss was 10.40%. C prepared in this example f / SiC-(Y 2 Si 2 o 7 ) 3 The flexural strength of the composite material is 422±21MPa.

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Abstract

The invention relates to a silicon carbide ceramic matrix composite material with layered distribution of rare earth silicates and a preparation method thereof. The SiC matrix of the body, the at least 2 layers of rare earth silicate layers distributed annularly between the fiber surface and the SiC matrix in the fiber preform, and the SiC layer between adjacent rare earth silicate layers; preferably, the The number of layers of the rare earth silicate layer is 2 to 3 layers.

Description

technical field [0001] The invention relates to a silicon carbide ceramic matrix composite material with layered distribution of rare earth silicate and a preparation method thereof, in particular to a silicon carbide ceramic matrix composite material with multilayer distribution of rare earth silicate in a ceramic matrix and the method of using rare earth salt The invention relates to a preparation method for synthesizing a silicon carbide ceramic matrix composite material with layered distribution of rare earth silicates by solution surface coating, dipping, pyrolysis and chemical vapor infiltration, belonging to the field of composite material preparation. Background technique [0002] With the increase of the unit thrust of the engine, the outlet temperature of the engine combustion chamber has been greatly increased, which puts forward higher requirements for the materials of the hot end components such as the combustion chamber and turbine. In the future, the temperatu...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B35/80C04B35/565C04B35/50C04B35/16
CPCC04B35/16C04B35/50C04B35/565C04B2235/3224C04B2235/3427C04B2235/3834C04B2235/5244C04B2235/5248C04B2235/656C04B2235/6567C04B2235/658C04B2235/6582C04B2235/95C04B2235/96C04B2235/9684
Inventor 张翔宇王鹏董绍明周海军杨金山阚艳梅胡建宝
Owner SHANGHAI INST OF CERAMIC CHEM & TECH CHINESE ACAD OF SCI