详细信息
Investigating the CMAS corrosion resistance and thermal cycling failure behavior of porous thermal barrier coatings with different morphologies prepared by plasma spraying ( SCI-EXPANDED收录 EI收录)
文献类型:期刊文献
英文题名:Investigating the CMAS corrosion resistance and thermal cycling failure behavior of porous thermal barrier coatings with different morphologies prepared by plasma spraying
作者:Zhang, Wenkang[1];Liu, Yangguang[1];Wang, Weize[1,2];Liu, Wei[1];Yang, Ting[1];Li, Kaibin[1];Wang, Junhao[1];Zhang, Xiaoqin[1];Wan, Jiangling[1];Zhang, Chengcheng[3]
机构:[1]East China Univ Sci & Technol, Key Lab Pressure Syst & Safety, Minist Educ, Shanghai 200237, Peoples R China;[2]Shanghai Inst Aircraft Mech & Control, Shanghai 200092, Peoples R China;[3]Aecc Commercial Aircraft Engine Co Ltd, Shanghai 200241, Peoples R China
年份:2024
卷号:489
外文期刊名:SURFACE & COATINGS TECHNOLOGY
收录:;EI(收录号:20240146479);WOS:【SCI-EXPANDED(收录号:WOS:001325502100001)】;
基金:This research was sponsored by National High Technology Research and Development Program of China (2023YFB3711200) , the National Natural Science Foundation of China (52175136, 52130511) , Science Center for Gas Turbine Project (P2021-A-IV-002) , Shanghai Joint Innovation Program in the Field of Commercial Aviation Engines, Shanghai Gaofeng Project for University Academic Program Development, and Key Research and Development Projects in Anhui Province (2022a05020004) .
语种:英文
外文关键词:Thermal barrier coating (TBCs); Embedded micro-agglomerated particle; (EMAP); Calcium-magnesium-aluminum-silicate; (CMAS); Thermal cycling-CMAS behavior; Mechanical properties
摘要:This study investigates the influence of two-phase powder feeding spacing on the thermal cycling and CMAS corrosion resistance of the thermal barrier coatings (TBCs). Porous thermal barrier coatings with varying microstructures were prepared using the embedded micro agglomerated particle (EMAP) coating preparation method, which is based on conventional yttrium stabilized zirconia (YSZ) coatings. The method involved changing the powder feeding spacing. TBCs' failure mode and microstructure are investigated under complex service conditions. The corrosion resistance, thermal cycling life, hardness, and elastic modulus of TBCs are investigated by thermal cycling-CMAS experiments and isothermal corrosion tests. The EMAP coating has a good service life in the thermal cycling-CMAS tests, with a lower hardness, lower elasticit modulus and larger surface roughness than conventional coatings. This research aims to provide a strategy to optimize structure for TBCs with excellent comprehensive performance.
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