首页|TC4合金表面Zr-Y改性渗硅涂层的组织结构及高温摩擦磨损性能

TC4合金表面Zr-Y改性渗硅涂层的组织结构及高温摩擦磨损性能

扫码查看
采用固体粉末扩散渗方法在TC4合金表面制备了Zr-Y改性的渗硅涂层,研究了渗层的组织结构、高温摩擦磨损性能及磨损机制.结果表明:Zr-Y改性渗硅涂层具有多层梯度结构,外层由TiSi2和少量ZrSi2组成,较薄的中间层为TiSi相,内层为Ti5Si4和Ti5Si3的混合物.涂层的显微硬度明显高于TC4合金基体,且由表及内呈梯度降低趋势.高温摩擦磨损实验(600℃)结果表明,Zr-Y改性渗硅涂层具有优良的摩擦磨损防护性能.与GCr15对磨时的磨损率约为3.59×10-5 mm3/(N·m),是相同条件下TC4合金磨损率的36.6%,磨损机制主要为GCr15在涂层表面的擦涂和氧化磨损.与Al2O3球对磨时的磨损率为9.75×10-5 mm3/(N·m),是相同条件下TC4合金磨损率的18.9%,磨损机制为疲劳磨损、氧化磨损和黏着磨损.
Microstructure and high-temperature wear performance of Zr-Y modified silicide coating deposited on TC4 alloy
Zr-Y modified silicide coating was deposited on TC4 alloy by the pack cementation process. The microstructure,friction and wear performance,and wear mechanisms of the coating were investigated. The results show that the Zr-Y modified silicide coating has a multi-layer structure,an outer layer consists of TiSi2 and a small amount of ZrSi2,a thin middle layer is TiSi,and an inner layer is a mixture of Ti5Si4 and Ti5Si3. The micro-hardness of the coating is much higher than that of the TC4 substrate and exhibits an obvious decrease tendency from the surface to the interior. The Zr-Y modified silicide coating possesses good anti-wear performance when wearing against GCr15 and Al2O3 balls at a high-temperature of 600 ℃. When wearing against GCr15,the wear rate of the coating is about 3.59×10-5 mm3/(N·m),which is about 36.6% of that of the TC4 substrate,and the main wear mechanisms are characterized by the adhesive of GCr15 on the coating surface and oxidation wear. When wearing against the Al2O3 ball,the wear rate of the coating is about 9.75×10-5 mm3/(N·m),which is about 18.9% of that of the TC4 substrate,and the wear mechanisms are fatigue wear,oxidation wear,and adhesion wear.

TC4 alloyZr-Y modificationdiffusion cementationsilicide coatinghigh-temperature wearwear mechanism

李轩、吕威、何瑜、张晓燕、贾丽娜、来升、袁泉

展开 >

四川轻化工大学机械工程学院,四川自贡 643000

西安长峰机电研究所,西安 710065

北京航空航天大学材料科学与工程学院,北京 100191

TC4合金 Zr-Y改性 扩散渗 硅化物涂层 高温磨损 磨损机制

国家自然科学基金项目四川省科技计划项目过程装备与控制工程四川省高校重点实验室开放课题项目

519610032022YFSY0036GK202202

2024

材料工程
中国航发北京航空材料研究院

材料工程

CSTPCD北大核心
影响因子:0.78
ISSN:1001-4381
年,卷(期):2024.52(6)