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Stellite12钴基合金的疲劳性能及其断裂机理研究
引用本文:苗文卷,曹睿,车洪艳,董浩,陈剑虹.Stellite12钴基合金的疲劳性能及其断裂机理研究[J].材料工程,2021,49(1):153-159.
作者姓名:苗文卷  曹睿  车洪艳  董浩  陈剑虹
作者单位:兰州理工大学 省部共建有色金属先进加工与再利用国家重点实验室,兰州 730050;兰州理工大学 材料科学与工程学院,兰州 730050;兰州理工大学 省部共建有色金属先进加工与再利用国家重点实验室,兰州 730050;兰州理工大学 材料科学与工程学院,兰州 730050;中国钢研科技集团有限公司 安泰科技股份有限公司,北京 100081;河北省热等静压工程技术研究中心,河北 涿州 072750;中国钢研科技集团有限公司 安泰科技股份有限公司,北京 100081;河北省热等静压工程技术研究中心,河北 涿州 072750;兰州理工大学 省部共建有色金属先进加工与再利用国家重点实验室,兰州 730050;兰州理工大学 材料科学与工程学院,兰州 730050
摘    要:采用三点弯曲疲劳法测得光滑试样和直缺口试样的S-N曲线以研究Stellite12钴基合金的疲劳性能,并通过断口形貌观察进一步探究该钴基合金的断裂过程。结果表明:光滑试样的疲劳极限为545 MPa,约为原始抗弯强度1552 MPa的25.4%;直缺口试样的疲劳极限约为101MPa,约为静态抗弯强度517.6MPa的19.1%。对于疲劳敏感性,光滑试样与直缺口试样的疲劳敏感性分别为397和31。此外发现疲劳裂纹多萌生于近表层聚集的碳化物处,同时表面缺陷也可诱发疲劳裂纹的萌生。疲劳裂纹的扩展主要表现为碳化物的穿晶断裂,钴基体在应力比R=0.1的疲劳加载条件下虽表现出一定的韧性且呈现出较多的撕裂脊,但也呈现出一定的脆性断裂模式,因此疲劳裂纹扩展模式为真疲劳与静态疲劳的混合模式。

关 键 词:三点弯曲疲劳  钴基合金  疲劳断裂  断裂模式

Fatigue properties and fracture mechanism of Stellite12 cobalt-based alloy
MIAO Wen-juan,CAO Rui,CHE Hong-yan,DONG Hao,CHEN Jian-hong.Fatigue properties and fracture mechanism of Stellite12 cobalt-based alloy[J].Journal of Materials Engineering,2021,49(1):153-159.
Authors:MIAO Wen-juan  CAO Rui  CHE Hong-yan  DONG Hao  CHEN Jian-hong
Affiliation:(State Key Laboratory of Advanced Processing and Recycling of Nonferrous Metals,Lanzhou University of Technology,Lanzhou 730050,China;School of Materials Science and Engineering,Lanzhou University of Technology,Lanzhou 730050,China;Advanced Technology&Materials Co.,Ltd.,China lron&Steel Research Institute Group,Beijing 100081,China;Hebei Province Engineering Research Center for Hot Isostatic Pressing,Zhuozhou 072750,Hebei,China)
Abstract:The three-point bending fatigue method was used to determine the S-N fatigue curves of smooth specimens and straight-notched specimens to study the fatigue properties of Stellite12 cobalt-based alloy, and the fatigue fracture processes of the cobalt-based alloy were investigated by the observation of fracture morphology.The results show that the fatigue limit of the smooth specimen is 545 MPa, which is about 25.4% of the original bending strength of 1552 MPa. The fatigue limit of the straight-notched specimen is about 101 MPa, which is about 19.1% of static bending strength of 517.6 MPa. The fatigue sensitivity of smooth specimens and straight-notched specimens is 397 and 31, respectively. In addition, it is found that the fatigue cracks can initiate in the carbides aggregated regions in the near surface. Surface defects can also induce the initiation of fatigue cracks. The transgranular fracture of the carbides dominates in the crack propagation. The cobalt base metal presents a lot of tearing ridges under the condition of stress ratio R=0.1, but it also shows a certain degree brittle fracture mode, so the fatigue crack propagation mode is a mixed mode of true fatigue and static fatigue.
Keywords:three point bending fatigue  cobalt-based alloy  fatigue fracture  fracture mode
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