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陶瓷基复合材料可磨耗环境障涂层制备及性能OA北大核心CSTPCD

Preparation and performance of abradable environmental barrier coating on ceramic matrix composites

中文摘要英文摘要

随着碳化硅陶瓷基复材制备的涡轮外环的逐步应用,与其匹配的可磨耗涂层技术需求迫切.本工作采用大气等离子喷涂技术,制备4层结构的BSAS(Ba0.75Sr0.25Al2Si2O8)-聚酯基可磨耗环境障涂层(A/EBCs),探究工艺参数对可磨耗面层孔隙率的影响规律以及涂层在1300℃下的相结构和组织演变.利用X射线衍射仪(XRD)、扫描电子显微镜(SEM)、能谱仪(EDS)、透射电镜(TEM)对涂层相结构、微观组织及成分进行分析表征.结果表明:BSAS-聚酯基可磨耗面层的孔隙率为 26.4%~36.8%,BSAS-聚酯粒子温度敏感的参量是主气(氩气)流量、辅气(氢气)流量和喷涂距离,速度敏感的参量是主气(氩气)流量;其中主气(氩气)流量同时对BSAS-聚酯的粒子温度和速度具有反向影响作用.该可磨耗面层在1300℃高温氧化300 h保持单斜相结构,组织和成分稳定,局部析出球状非晶氧化硅颗粒.采用高温高速刮削实验对涂层可磨耗性能进行评价,涂层表面发现纳米高温合金微粒黏附,叶片高度磨损比(IDR)为20%,达到可磨耗封严涂层使用要求.

With the application of shrouds made of silicon carbide ceramic matrix composite(SiC-CMCs),the abradable coating technology suitable for SiC-CMCs is urgently needed.The four-layer structure of BSAS(Ba0.75Sr0.25Al2Si2O8)-polyester-based abradable environmental barrier coating(A/EBCs)was prepared by atmospheric plasma spraying.The influence of process parameters on the porosity and the structural evolution of the layer at 1300℃ were investigated.The phase structure,microstructure and coating composition were characterized by XRD,SEM,EDS and TEM respectively.The results show that the porosity of BSAS-polyester abradable top layer is 26.4%-36.8%.And the temperature-sensitive parameters of BSAS-polyester particles are primary gas(argon)flow,second gas(hydrogen)flow and spraying distance.In contrast,the speed-sensitive parameters are primary gas(argon)flow.The primary gas(argon)flow has the opposite effect on the particle temperature and velocity of the BSAS-polyester.The abradable surface layer is oxidized at 1300℃for 300 h and maintains monoclinic phase structure,stable stucture and composition,and locally precipitates spherical amorphous silicon oxide particles.Furthermore,the coating abradability was evaluated by high-temperature and high-speed scraping test.Nano-scale Ni-based superalloy particles adhesion on the surface of the coating are found,and the blade incursion depth ratio(IDR)is 20%,which meets the requirements of the abradable sealing coating.

袁世峰;郭婧;郭孟秋;赵春玲;崔永静;焦健

中国航发湖南动力机械研究所,湖南株洲 412002中国航发北京航空材料研究院,北京 100095

可磨耗环境障涂层等离子喷涂碳化硅陶瓷基复合材料BSAS高温性能

abradable environmental barrier coating(A/EBCs)plasma sprayingsilicon carbide ceramic matrix composites(SiC-CMCs)BSAShigh temperature performance

《航空材料学报》 2024 (003)

82-94 / 13

航空发动机及燃气轮机基础科学中心项目(P2022-B-Ⅳ-003-001)

10.11868/j.issn.1005-5053.2023.000185

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