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基于力-热耦合仿真模型的切削引入残余应力形成规律研究OA

Research on the Formation Law of Residual Stress Induced by Cutting Based on Mechanical and Thermal Coupling Simulation Model

中文摘要英文摘要

金属切削加工方式是多因素多物理场耦合、涉及材料大变形、高度非线性的减材加工过程,为了实现切削加工过程的数字化、信息化、智能化,本文研究了切削材料的本构模型,利用AdvantEdge和Abaqus建立了切削过程的力-热耦合数值仿真分析模型,利用切削试验验证了有限元模型的正确性、可靠性,通过正交试验分析了主轴转速、切削速度、铣削深度、铣削宽度4个因素对切削力、表面温度、表面残余应力的影响.结果表明,切削开始时切削部位温度急剧升高导致切削表面产生剧烈的热-弹塑性变形,这是引起残余应力生产的主要原因,针对固溶处理与时效处理后的7050铝合金厚板,发现切削速度对表面残余应力的影响最大,得到了其表面残余应力最小的切削参数分别为:进给速度为1200mm/min,铣削深度为0.5mm,铣削宽度为12mm,主轴转速为4000r/min.本文为7050铝合金薄壁结构零件在切削加工中表面残余应力的分析提供了一种新方法,为航空航天领域的薄壁结构零件的高精度制造提供了理论基础.

The metal cutting process is a highly nonlinear material reduction process with coupling of multiple factors and multiple physical fields,involving large deformation of materials.In order to realize the digitization,informatization and intellectualization of cutting process,this paper studies the constitutive model of cutting materials.AdvantEdge and Abaqus are used to establish a numerical simulation analysis model of mechanical and thermal coupling in cutting process.Cutting tests are used to verify the correctness and reliability of the finite element model.Through orthogonal tests,the influence on spindle speed,cutting speed,milling depth and milling width on cutting force,surface temperature and surface residual stress are analyzed.The results show that the sharp temperature rise at the cutting position at the beginning of cutting results in intense thermo-elastoplastic deformation on the cutting surface,which is the main cause of residual stress production.For 7050 aluminum alloy thick plate after solution treatment and aging treatment,it is found that the cutting speed has the greatest impact on the surface residual stress.The minimum cutting parameters of the surface residual stress are:feed speed of 1200mm/min,milling depth of 0.5mm,milling width of 12mm and spindle speed of 4000r/min.This paper provides a new method to analyze the surface residual stress of 7050 aluminum alloy thin-wall structural parts in cutting process,and provides a theoretical basis for high-precision manufacturing of thin-wall structural parts in aerospace field.

闫坤;李昕;赵勇博;张文宣;高瀚君;吴琼

北京航空航天大学,北京 100191||北京航空航天大学江西研究院景德镇分院,江西 景德镇 333000中国航空研究院,北京 100012

机械工程

切削加工力-热耦合数值仿真正交试验表面残余应力

cutting processingmechanical and thermal couplingnumerical simulationorthogonal testsurface residual stress

《航空科学技术》 2024 (009)

35-44 / 10

航空科学基金(2019ZE051002) National Aeronautical Science Foundation of China(2019ZE051002)

10.19452/j.issn1007-5453.2024.09.004

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