High temperature resistant ceramic matrix composite material and preparation method thereof
A technology of ultra-high temperature ceramics and composite materials, which is applied in the field of ultra-high temperature resistant ceramic matrix composite materials and its preparation technology, can solve the problems of difficult forming of large and complex components, poor reliability, and poor thermal shock resistance of materials, and achieve excellent thermal resistance. seismic performance, high reliability, high fracture toughness effect
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Embodiment 1
[0019] A 2D C / ZrB 2 -SiC ultra-high temperature resistant ceramic matrix composite material, the composite material uses two-dimensional carbon fiber cloth as a reinforcing phase, and a high melting point boride (ZrB 2 ) ceramic powder as the filler, silicon carbide as the matrix, wherein the volume fraction of carbon fibers in the reinforcing phase is 25.45%, and the filler ZrB 2 The volume fraction of the powder is 20.33%, the volume fraction of the SiC matrix is 35%, and the porosity is 19.22%.
[0020] 2D C / ZrB above 2 -SiC ultra-high temperature resistant ceramic matrix composite material is prepared through the following steps:
[0021] (1) PCS, divinylbenzene, and xylene were formulated into a mixed solution at a mass ratio of 1:0.3:0.5, and then the mixed solution was mixed with ZrB 2 The powders were mixed at a volume ratio of 1:3, and ball milled for 8 hours to form a slurry;
[0022] (2) Cut the 3K carbon fiber cloth produced by Jilin Carbon Factory into cloth...
Embodiment 2
[0028] A 2D C / TaC-SiC ultra-high temperature resistant ceramic matrix composite material, the composite material uses two-dimensional carbon fiber cloth as a reinforcing phase, uses high melting point carbide (TaC) ceramic powder as a filler, and uses silicon carbide as a matrix, wherein The volume fraction of reinforcing phase carbon fiber is 20.5%, the volume fraction of filler TaC powder is 40.0%, the volume fraction of SiC matrix is 34.3%, and the porosity is 5.2%.
[0029] The above-mentioned 2D C / TaC-SiC ultra-high temperature resistant ceramic matrix composite material is prepared through the following steps:
[0030] (1) PCS and divinylbenzene are formulated into a mixed solution with a mass ratio of 1:1, then the mixed solution and TaC powder are mixed with a volume ratio of 1:4, and ball milled for 8 hours to form a slurry;
[0031] (2)-(5) are the same as steps (2)-(5) of Example 1.
[0032] The density of the final 2D C / TaC-SiC ultra-high temperature resistant c...
Embodiment 3
[0034] A 2D C / ZrB 2 -C ultra-high temperature resistant ceramic matrix composite material, the composite material uses two-dimensional carbon fiber cloth as a reinforcing phase, and a high melting point boride (ZrB 2 ) ceramic powder as a filler, with carbon as a matrix, wherein the volume fraction of carbon fibers in the reinforcing phase is 44.8%, and the filler ZrB2 The volume fraction of the powder is 5.6%, the volume fraction of the C matrix is 35%, and the porosity is 14.6%.
[0035] 2D C / ZrB above 2 -C ultra-high temperature resistant ceramic matrix composite material is prepared through the following steps:
[0036] (1) Prepare a mixed solution with phenolic resin and acetone at a ratio of 1:1, and then mix the mixed solution with ZrB 2 The powders were mixed at a volume ratio of 1:1, and ball milled for 8 hours to form a slurry;
[0037] (2) and (3) are identical with the steps (2) and (3) of embodiment 1;
[0038] (4) put the above-mentioned cracked sample into...
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