摘要
Dry wear tests under atmospheric conditions at 25-200 °C and loads of 12.5-300 N were performed for AM60B alloy. The wear rate increases with increasing the load; the mild-to-severe wear transitions occur under the loads of 275 N at 25 °C, 150 N at 100 °C and 75 N at 200 °C, respectively. However, as the load is less than 50 N, the wear rate at 200 °C is lower than that at 25 °C or 100 °C. In mild wear regimes, the wear mechanisms can be classified into abrasive wear, oxidation wear and delamination wear. Delamination wear prevailed as the mild-to-severe wear transition starts to occur; the delamination occurs from the inside of matrix. Subsequently, plastic-extrusion wear as severe wear prevails accompanied with the transition. The thick and hard tribo-layer postpones the mild-to-severe wear transition due to restricting the occurrence of massive plastic deformation of worn surfaces.
针对AM60B合金在环境温度25～200℃、载荷12.5～300N的条件下进行干摩擦磨损实验。结果表明:随着载荷的增大,磨损率增加;从轻微磨损到严重磨损的转变的临界载荷分别为25℃时275N,100℃时150N,200℃时75N。在低载荷(<50N)下,200℃下的磨损率低于25℃和100℃的。在轻微磨损阶段,磨损机制为磨粒磨损、氧化磨损和剥层磨损。当轻微磨损到严重磨损的转变开始时,剥层磨损发挥主要作用,剥层磨损是从基体内部发生的剥落。随后,塑性挤出磨损作为严重磨损出现,同时伴随着从轻微磨损到严重磨损的转变。厚的、硬的摩擦层通过限制磨面的塑性变形来阻碍从轻微磨损到严重磨损的转变。
基金
Project (51071078) supported by the National Natural Science Foundation of China
Project (AE201035) supported by the Research Fund of Key Laboratory for Advanced Technology in Environmental Protection of Jiangsu Province, China
