OVERHEATING

作品数：43被引量：42H指数：4
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相关领域：经济管理更多>>
相关作者：肖晓燕杨梦琳刘新才潘晶更多>>
相关机构：清华大学宁波大学更多>>
相关期刊：《Journal of Magnesium and Alloys》《Journal of Arid Land》《Chinese Physics B》《Journal of Energy Chemistry》更多>>
相关基金：国家自然科学基金安徽省自然科学基金高等学校学科创新引智计划更多>>
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Solid dust induced roughening and overheating of TBC-coated superalloy
《Journal of Materials Science & Technology》2024年第13期69-79,共11页Jia-Qi Han Mei-Jun Liu Javad Mostaghimi Guan-Jun Yang 
National Natural Science Foundation of China(No.51901175);China Postdoctoral Science Foundation Grant(Nos.2020T130499 and 2019M653602);HPC platform in Xi'an Jiaotong University.
Thermal barrier coatings(TBC)on superalloy blade/vane enable an increase in turbine inlet temperature(TIT)and aero-engine efficiency.However,the deposition of dust on TBC significantly ablates superalloys and becomes ...
关键词：Thermal barrier coating SUPERALLOY DUST ROUGHNESS OVERHEATING 
Thermal cycling creep properties of a directionally solidified superalloy DZ125被引量：3
《Journal of Materials Science & Technology》2022年第9期269-284,共16页Wenrui An Satoshi Utada Xiaotong Guo Stoichko Antonov Weiwei Zheng Jonathan Cormier Qiang Feng 
supported by the“National Key Research and Development Program of China(Grant No.2016YFB0701403)”;the“National Natural Science Foundation of China(Grant Nos.51631008 and 91860201)”;the“111 Project(No.B170003)”;financial support to the reported work.Stoichko Antonov would like to acknowledge financial support from the Alexander von Humboldt Foundation。
Aero-engine turbine blades may suffer overheating during service,which can result in severe microstructural and mechanical degradation within tens of seconds.In this study,the thermal cycling creep under(950℃/15 min+...
关键词：Directional solidified superalloy Thermal cycling creep OVERHEATING Creep properties Microstructural degradation 
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