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作 者:Desheng HU Caixu YUE Xianli LIU Zhipeng JIANG Yongshi XU Junhui LU Steven Y.LIANG
机构地区:[1]Key Laboratory of Advanced Manufacturing and Intelligent Technology,Ministry of Education,Harbin University of Science and Technology,Harbin 150080,China [2]George W.Woodruff School of Mechanical Engineering,Georgia Institute of Technology,Atlanta 30332,USA
出 处:《Chinese Journal of Aeronautics》2024年第11期477-492,共16页中国航空学报(英文版)
基 金:supported by the Natural Science Foundation of Heilongjiang Province(No.TD2022E003);the National Natural Science Foundation of China(No.52175393)。
摘 要:42CrMo steel has the characteristics of high strength,high wear resistance,high impact resistance,and fatigue resistance.Therefore,drilling 42CrMo steel has always been a challenging task.The indexable drill bit has the advantages of high processing efficiency and low processing cost and has been widely used in the field of aerospace hole processing.To better understand the machining mechanism of the indexable drill bit,this paper uses the Coupled EulerianLagrangian method(CEL)to simulate the three-dimensional drilling model for the first time.The simulation results of the drilling force obtained by the CEL method and Lagrangian method are compared with the experimental results.It is verified that the CEL method is easy to converge and can avoid the problem of program interruption caused by mesh distortion,and the CEL simulation value is more consistent with the actual value.Secondly,the simulation results of cutting force and blade cutting edge node temperature under different process parameters are extracted.The variation of time domain cutting force,frequency domain cutting force and tool temperature with process parameters are obtained.This study provides a new method for the prediction of cutting performance and the optimization of process parameters of indexable drills.
关 键 词:42CrMo steel Coupled EulerianLagrangian method Indexable drill bit Drilling force Process parameters
分 类 号:V263[航空宇航科学与技术—航空宇航制造工程]
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