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Self-healing SiC/ZrSi2-MoSi2 coating material and preparation method thereof

A coating material and self-healing technology, applied in the field of SiC/ZrSi2-MoSi2 composite ceramic coating, self-healing SiC/ZrSi2-MoSi2 coating material and preparation, can solve the problem of large glass phase, limited content and influence Coating protection effect, etc.

Active Publication Date: 2017-08-11
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in the process of plasma spraying, high temperature will make SiO with low melting point 2 Volatile, remaining SiO in the coating 2 Limited content, difficult to heal larger holes and cracks in the coating
In addition, borides formed at a high temperature of 1450 ° C 2 o 3 Violent volatilization will form larger holes in the glass phase, affecting the protective effect of the coating

Method used

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  • Self-healing SiC/ZrSi2-MoSi2 coating material and preparation method thereof
  • Self-healing SiC/ZrSi2-MoSi2 coating material and preparation method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment example 1

[0036] Step 1: Cut the C / C Composite into 10×10×10mm 3 The small pieces were ultrasonically cleaned with absolute ethanol for 1 h, and then dried in a blast drying oven at 80 °C for 2 h for later use.

[0037] Step 2: Prepare a SiC transition layer on the surface of the C / C composite material, the specific process is:

[0038] 1) Prepare the powder required for the embedding method: weigh 65g of silicon powder (300 mesh), 20g of carbon powder (300 mesh) and 15g of alumina powder (300 mesh) respectively, and pour in zirconia at the same time In a ball mill tank, mix at a speed of 200r / min for 2 hours to obtain a uniformly mixed embedding raw material powder;

[0039] 2) Embedding infiltration: Lay several layers of graphite paper inside the graphite crucible, and then embed the C / C composite material sample obtained in step 1 into the mixed embedding raw materials in the crucible. Put the prepared crucible in a high-temperature graphitization heat treatment furnace for 2 hour...

Embodiment example 2

[0045] Step 1: Cut the C / C Composite into 10×10×10mm 3 The small pieces were ultrasonically cleaned with absolute ethanol for 1 h, and then dried in a blast drying oven at 80 °C for 2 h for later use.

[0046] Step 2: Prepare a SiC transition layer on the surface of the C / C composite material, the specific process is:

[0047] 1) Prepare the powder required for the embedding method: weigh silicon powder (300 mesh) with a mass fraction of 80, carbon powder (300 mesh) with a mass fraction of 10 and alumina powder (300 mesh) with a mass fraction of 10g, and pour in zirconia at the same time In a ball mill tank, mix at a speed of 200r / min for 2 hours to obtain a uniformly mixed embedding raw material powder;

[0048] 2) Embedding infiltration: Lay two layers of graphite paper inside the graphite crucible, and then embed the C / C composite material sample obtained in step 1 into the mixed embedding raw materials in the crucible. The prepared crucible was placed in a high-temperatu...

Embodiment example 3

[0054] Step 1: Cut the C / C Composite into 10×10×10mm 3 The small pieces were ultrasonically cleaned with absolute ethanol for 1 h, and then dried in a blast drying oven at 80 °C for 2 h for later use.

[0055] Step 2: Prepare a SiC transition layer on the surface of the C / C composite material, the specific process is:

[0056] 1) Prepare the powder required for the embedding method: weigh 70g of silicon powder (300 mesh), 20g of carbon powder (300 mesh) and 10g of alumina powder (300 mesh) respectively, and pour in zirconia at the same time In a ball mill tank, mix at a speed of 200r / min for 2 hours to obtain a uniformly mixed embedding raw material powder;

[0057] 2) Embedding infiltration: Lay two layers of graphite paper inside the graphite crucible, and then embed the C / C composite material sample obtained in step 1 into the mixed embedding raw materials in the crucible. The prepared crucible was placed in a high-temperature graphitization heat treatment furnace for 2 h...

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Abstract

The invention relates to a self-healing SiC / ZrSi2-MoSi2 coating material and a preparation method thereof. The self-healing SiC / ZrSi2-MoSi2 coating material is characterized by being prepared from, by mass percentage, 20-50% of ZrSi2 and 50-80% of MoSi2. The preparation method is characterized in that evenly distributed ZrSi2 is introduced into MoSi2 ceramic to allow the crack size of thermal-spraying ceramic coating to be reduced from 8.3 micrometers to 4.5 micrometers; the ZrSi2 serving as the self-healing phase can be oxidized for 3-10 hours under the high temperature condition of 1450 DEG C to generate an SiO2 glass mobile phase to heal cracks, ZrO2 is generated at the same time, and the ZrO2 has volume expansion and generates pressure stress in the coating to inhibit crack generation in a cooling process. Compared with a traditional method, the preparation method has the advantages that the oxidation resistance of the prepared self-healing SiC / ZrSi2-MoSi2 ceramic coating is increased from 2.24% of weight loss in 29 hours to 1.89% of weight gain in 41 hours, the section of the coating has no evident defects, and the self-healing coating can be used as the high-temperature coating material of C / C composite materials.

Description

technical field [0001] The invention belongs to the technical field of self-healing coating materials, and relates to a self-healing SiC / ZrSi 2 -MoSi 2 Coating material and preparation method, specifically relate to a kind of by introducing alloy component ZrSi 2 Fabrication of SiC / ZrSi with self-healing properties 2 -MoSi 2 Method for multiphase ceramic coatings. Background technique [0002] As a high-temperature thermal structural material, C / C composite materials have broad application prospects in aerospace and other fields. However, they will be oxidized and corroded in an oxygen-containing atmosphere higher than 400 ° C, which will seriously affect the performance of the material. The preparation of high-temperature coatings is a solution efficient approach to the problem. MoSi 2 Ceramics have excellent high-temperature oxidation resistance and are one of the candidate materials for coatings. However, ceramic materials have the shortcomings of high brittleness ...

Claims

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Application Information

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IPC IPC(8): C04B35/58C04B35/622C04B41/87
CPCC04B35/58092C04B35/62222C04B41/009C04B41/5071C04B41/87C04B2235/3891C04B41/4543C04B35/83
Inventor 付前刚王璐赵凤玲李贺军李克智
Owner NORTHWESTERN POLYTECHNICAL UNIV