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FATIGUE OF ALUMINA-CHROME CARBIDE COMPOSITE COATING

机译:铝铬合金复合涂层的疲劳

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摘要

The fracture and fatigue characteristics of alumina coating strengthen with chrome carbide layer, is presented and discussed. The essential aspects of the methodology include acoustic emission monitoring of crack activity and its propagation under cyclic loads. Structural analysis of the alumina revealed an effect of α, γ phases of alumina and CrC thickness on fatigue life of the coating. The fatigue life of the coatings is found to be no longer than 10~3 cycles. None of the coatings resist above 10~3 cycles. It is found to be cracks initiation and propagation in the coating interface that result in the catastrophic failure of the composite. An ultimate load resulted in intensive crack growth in CrC-Al_2O_3-Al is found to be about 2 GPa that is higher than that in alumina coating.
机译:介绍并讨论了碳化铬层增强氧化铝涂层的断裂和疲劳特性。该方法的基本方面包括对裂纹活动及其在循环载荷下的传播进行声发射监测。氧化铝的结构分析表明,氧化铝的α,γ相和CrC厚度对涂层的疲劳寿命有影响。涂层的疲劳寿命不超过10〜3个循环。没有一个涂层能抵抗10〜3次以上的循环。发现是在涂层界面的裂纹萌生和扩展,其导致复合材料的灾难性破坏。最终载荷导致CrC-Al_2O_3-Al的剧烈裂纹扩展,约为2 GPa,比氧化铝涂层的高。

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