航空发动机热障涂层的CMAS腐蚀行为与防护方法
CMAS Corrosion Behavior and Protection Method of Thermal Barrier Coatings for Aeroengine
(a, b) single layer fracture cross-sections (c, d) double layer surfaces (e, f) double layer fracture cross-sections
航空发动机热障涂层的CMAS腐蚀行为与防护方法 |
| 郭磊, 高远, 叶福兴, 张馨木 |
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CMAS Corrosion Behavior and Protection Method of Thermal Barrier Coatings for Aeroengine |
| GUO Lei, GAO Yuan, YE Fuxing, ZHANG Xinmu |
| 图6 激光改性涂层后单层断面形貌和双层的表面及断面形貌 (a, b) single layer fracture cross-sections (c, d) double layer surfaces (e, f) double layer fracture cross-sections |
| Fig.6 Surface and fracture cross-sectional morphologies of laser-glazed coatings before (a, c, e) and after (b, d, f) parameter optimization |
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