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NiCrAlYSi/h-BN高温可磨耗封严涂层摩擦磨损性能研究
引用本文:运广涛,李其连,程旭东.NiCrAlYSi/h-BN高温可磨耗封严涂层摩擦磨损性能研究[J].表面技术,2016,45(2):103-108,174.
作者姓名:运广涛  李其连  程旭东
作者单位:武汉理工大学 材料复合新技术国家重点实验室,武汉430070;北京航空制造工程研究所 高能束流加工技术重点实验室,北京100024;北京航空制造工程研究所 高能束流加工技术重点实验室,北京,100024;武汉理工大学 材料复合新技术国家重点实验室,武汉,430070
摘    要:目的加入h-BN和团聚聚苯酯分别作为固体润滑剂和造孔剂,以提高NiCrAlYSi基封严涂层的高温摩擦磨损性能。方法采用真空熔炼雾化造粒和料浆喷雾造粒技术制备NiCrAlYSi/h-BN聚苯酯复合粉体,再利用大气等离子喷涂技术制备高温可磨耗封严涂层,通过扫描电子显微镜(SEM)、能谱仪(EDS)、CSM摩擦磨损试验机和三维轮廓仪等手段,研究NiCrAlYSi/h-BN封严涂层显微结构、元素组成以及室温和800℃下的摩擦磨损性能,探究涂层在室温和800℃下的磨损机理。结果等离子喷涂NiCrAlYSi/h-BN封严涂层组织比较均匀,涂层结合强度可达15MPa,孔隙率约为32%。室温下封严涂层与DD6镍基单晶高温合金球间的平均摩擦因数为0.897,涂层磨损体积为2.09×10~8μm~3;800℃高温下平均摩擦因数为0.425,涂层磨损体积为3.22×10~8μm~3;封严涂层800℃下有良好的可磨耗性,相应对偶件的磨损较轻;高温下,封严涂层金属基相软化、h-BN的润滑作用和部分金属基相高温下生成自润滑性氧化物,是摩擦因数降低和对偶件磨损较轻的主要原因。NiCrAlYSi/h-BN封严涂层室温的主要磨损机理为涂抹、磨粒磨损和轻微氧化,高温下的主要磨损机理为切削、塑性变形、氧化和粘着磨损。结论等离子喷涂NiCrAlYSi/h-BN高温封严涂层在高温下的可磨耗性能较好。

关 键 词:等离子喷涂  NiCrAlYSi/h-BN封严涂层  组织形貌  可磨耗性能  磨损机理
收稿时间:2015/11/18 0:00:00
修稿时间:2016/2/20 0:00:00

Friction and Wear Properties of NiCrAlYSi / h-BN High-temperature Abradable Seal Coatings
YUN Guang-tao,LI Qi-lian and CHENG Xu-dong.Friction and Wear Properties of NiCrAlYSi / h-BN High-temperature Abradable Seal Coatings[J].Surface Technology,2016,45(2):103-108,174.
Authors:YUN Guang-tao  LI Qi-lian and CHENG Xu-dong
Affiliation:1. State Key Laboratory of Advanced Technology for Materials Synthesis and Progressing, Wuhan University of Technology, Wuhan 430070, China; 2. Laboratory of Science and Technology on Power Beam Processes, Beijing Aeronautical Manufacturing Technology Research Institute, Beijing 100024, China,Laboratory of Science and Technology on Power Beam Processes, Beijing Aeronautical Manufacturing Technology Research Institute, Beijing 100024, China and State Key Laboratory of Advanced Technology for Materials Synthesis and Progressing, Wuhan University of Technology, Wuhan 430070, China
Abstract:Objective To improve the tribological properties of the NiCrAlYSi based seal coatings by adding h-BN and polyester into the coatings as lubrication and pore forming material, respectively. Methods The NiCrAlYSi/h-BN/ polyester composite pow-der was prepared by the technology of vacuum melting atomization and spray granulation. The NiCrAlYSi/h-BN high-temperature abradable seal coatings were prepared by atmospheric plasma-spray technology. The microstructure, elements and tribological prop-erties at room temperature and 800℃ of coatings were studied by SEM,EDS,CSM tribometer and three-dimensional contour instru-ment. The tribological mechanisms of the coatings were investigated at room temperature and 800 ℃. Results The NiCrAlYSi/h-BN abradable seal coatings had uniform microstructure and the tensile strength of the coatings was about 15 MPa. The porosity of the coating was about 32%. The room-temperature average friction coefficient between NiCrAlYSi/h-BN and DD6 alloy ball was 0. 897, and the average friction coefficient at 800 ℃ was 0. 425. The wear volume of the coatings at room-temperature and 800 ℃was 2. 09×108 μm3 and 3. 22×108 μm3, respectively. The wear performance of the coating at 800 ℃ was good and the abrasion of DD6 alloy ball was slight, which was due to the softened metal matrix phase, the lubrication of h-BN lubricant material and the for-mation of metallic self-lubricant oxide at high temperature. The main room-temperature wear mechanisms of NiCrAlYSi/h-BN coa-ting were smearing, particle wear and slight tribo-oxidation; while the main wear mechanisms at high temperature were cutting, plastic deformation, tribo-oxidation and adherence wear. Conclusion The NiCrAlYSi/h-BN high temperature abradable seal coa-tings exhibited excellent wear performance at high temperature.
Keywords:plasma spray  NiCrAlYSi / h-BN seal coatings  microstructure  abradability  wear mechanisms
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