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摘要:
During flight, many silicates (sand, dust, debris, fly ash, etc.) are ingested by an engine. They melt at high operating temperatures on the surface of thermal barrier coatings (TBCs) to form calcium–magnesium–aluminum–silicate (CMAS) amorphous settling. CMAS corrodes TBCs and causes many problems, such as composition segregation, degradation, cracking, and disbanding. As a new generation of TBC candidate materials, rare-earth zirconates (such as Sm2Zr2O7) have good CMAS resistance properties. The reaction products of Sm2Zr2O7 and CMAS and their subsequent changes were studied by the reaction of Sm2Zr2O7 and excess CMAS at 1350℃. After 1 h of reaction, Sm2Zr2O7 powders were not completely corroded. The reaction products were Sm–apatite and c-ZrO2 solid solution. After 4 h of reaction, all Sm2Zr2O7 powders were completely corroded. After 24 h of reaction, Sm–apatite disappeared, and the c-ZrO2 solid solution remained.
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篇名 Reaction products of Sm2Zr2O7 with calcium–magnesium– aluminum–silicate (CMAS) and their evolution
来源期刊 先进陶瓷(英文版) 学科
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年,卷(期) 2021,(6) 所属期刊栏目 Research Article
研究方向 页码范围 1389-1397
页数 9页 分类号
字数 语种 英文
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先进陶瓷(英文版)
季刊
2226-4108
10-1154/TQ
eng
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290
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157
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