Erosion resistance of a combined multilayer coating protecting critical parts of modern gas turbine engines

B. Guzanov, N. B. Pugacheva, T. Bykova
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Abstract

Comprehensive studies of the chemical composition, microstructure, and thickness of a combined multilayer coating on a heat-resistant nickel alloy are presented. The distribution pat-tern of chemical elements over the coating thickness for all the layers, namely the inner aluminosili-cated layer, the plasma sublayer, and the outer heat-insulating layer, has been established. Surface roughness was determined at all the stages of coating application and after testing. The results of comparative tests of corrosion-erosion resistance and resistance to burn-through of a diffusion aluminosilicide coating, a two-layer heat-insulating coating, and a combined multilayer coating are presented. High heat-shielding properties of a combined multilayer coating on a heat-resistant nickel alloy have been discovered.
现代燃气涡轮发动机关键部件复合多层涂层的抗侵蚀性能
对耐热镍合金复合多层涂层的化学成分、显微组织和厚度进行了全面的研究。建立了化学元素在涂层厚度上的分布规律,即内层硅酸铝层、等离子体亚层和外层隔热层。在涂层应用的所有阶段和测试后测量表面粗糙度。介绍了扩散型硅化铝涂层、双层隔热涂层和多层复合隔热涂层的耐蚀性和耐烧透性对比试验结果。发现了耐热镍合金复合多层涂层的高热屏蔽性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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