的个人主页 http://faculty.nuaa.edu.cn/xuweizheng/zh_CN/index.htm
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所属单位:航天学院
发表刊物:Chin J Aeronaut
摘要:Residual stresses produced in polycrystalline CBN abrasive grits during a high-frequency induction brazing process are calculated by using finite element analysis, with a consideration of the nonuniform temperature distribution in the induction brazing model. The influences of induction brazing parameters on the residual stresses of polycrystalline CBN abrasive grits have been analyzed, including the embedding depth, grit side length, etc. Results obtained show that the tensile stress with a 40% embedding depth is 292 MPa, which is the minimum on the bonding interface compared with other embedding depths. Meanwhile, the maximum tensile stress is 575 MPa, with an increase of 59% compared with that of a grit side length of 50 mm. Finally, the simulation results of the brazing residual stress of polycrystalline CBN abrasive grits have been confirmed valid based on the residual stress measurement of the brazed monocrystalline CBN grit. © 2018 Chinese Society of Aeronautics and Astronautics
ISSN号:1000-9361
是否译文:否
发表时间:2019-04-01
合写作者:XU, Wei,ZHU, Yejun,DU, Baicun,丁文锋
通讯作者:XU, Wei,徐伟证