Method for detecting high temperature thermal shock resistance of composite material
Patent Information
- Authority / Receiving Office
- CN ยท China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH
- Publication Date
- 2019-03-26
- Estimated Expiration
- Not applicable ยท inactive patent
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Abstract
Description
technical field
[0001] The invention relates to the technical field of material performance testing, in particular to a method for testing the high temperature thermal shock resistance performance of composite materials. Background technique
[0002] Carbon fiber toughened ceramic matrix composites (such as C / SiC, C / ZrC and multi-component ceramic matrix) have the characteristics of low thermal expansion coefficient and moderate elastic modulus, so they have excellent thermal shock resistance and are mainly used in aerospace High temperature thermal structural materials in the field.
[0003] At present, the evaluation methods for high temperature oxidation resistance of such materials mainly include oxygen-acetylene flame ablation, plasma arc ablation and combustion wind tunnel. The above three methods can be used for material screening and performance comparison. Among them, the basic principle of oxygen-acetylene flame ablation is: use the oxygen-acetylene flame flow as ...