共查询到19条相似文献,搜索用时 87 毫秒
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为了研究不同铣削参数对7075铝合金铣削过程中铣削力和铣削温度的影响,进行铣削参数优化。采用仿真与试验验证结合的方法,利用有限元建立2D铣削仿真模型,研究铣削过程中铣削力和铣削温度的变化,并在相同的切削条件下进行铣削试验测量铣削力,通过正交试验和单因素试验进行铣削参数优化。结果表明,有限元仿真结果与试验结果数据相近,验证了有限元模型的准确性,通过正交试验选出最优的铣削工艺参数为主轴转速6000r/min、每齿进给量0.05mm/z、铣削宽度2mm、铣削深度0.5mm;铣削7075铝合金时,在不影响生产的条件下,应采用较高的主轴转速,较低的进给量、铣削深度和铣削宽度,铣削温度随每齿进给量、主轴转速和铣削宽度升高而变大,铣削深度对铣削温度的影响极小。 相似文献
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为研究切削用量对微细铣削7075铝合金切削力的影响,采用正交试验法进行微细铣削7075铝合金的切削仿真研究,得到多组不同的切削力。对微细铣削仿真结果进行极差分析,得到切削用量对切削力影响程度的主次顺序及最优切削方案。通过微细铣削7075铝合金的切削试验,将仿真和试验结果作对比分析,验证了微细铣削仿真模型的准确性及合理性。在此加工仿真模型基础上,进一步采用单因素试验法进行了微细铣削仿真,分析了微细铣削7075铝合金时不同切削用量对切削力的影响规律。研究结果表明:切削用量影响微细铣削7075铝合金切削力的主次顺序从大到小依次为背吃刀量、切削速度和每齿进给量;背吃刀量与切削力成正比,切削速度则与之成反比。 相似文献
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针对玻璃纤维增强复合材料(GFRP)进行铣削力研究,以切削参数(主轴转速、进给速度、进给量)为自变量进行L_(27)(3~(13))正交试验,分析其对GFRP铣削力的影响。试验表明,铣削力随进给速度、铣削深度的增大而增大,随主轴转速的增大而减小。对铣削力做多元回归分析,建立相关数学模型并通过显著性分析验证其合理性,有助于分析切削参数对铣削力的影响规律。 相似文献
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Zhenjing Duan Changhe Li Wenfeng Ding Yanbin Zhang Min Yang Teng Gao Huajun Cao Xuefeng Xu Dazhong Wang Cong Mao Hao Nan Li Gupta Munish Kumar Zafar Said Sujan Debnath Muhammad Jamil Hafiz Muhammad Ali 《机械工程学报(英文版)》2021,34(1):54-88
Aluminum alloy is the main structural material of aircraft,launch vehicle,spaceship,and space station and is pro-cessed by milling.However,tool wear and vibration are the bottlenecks in the milling process of aviation aluminum alloy.The machining accuracy and surface quality of aluminum alloy milling depend on the cutting parameters,material mechanical properties,machine tools,and other parameters.In particular,milling force is the crucial factor to determine material removal and workpiece surface integrity.However,establishing the prediction model of milling force is important and difficult because milling force is the result of multiparameter coupling of process system.The research progress of cutting force model is reviewed from three modeling methods:empirical model,finite element simulation,and instantaneous milling force model.The problems of cutting force modeling are also determined.In view of these problems,the future work direction is proposed in the following four aspects:(1)high-speed milling is adopted for the thin-walled structure of large aviation with large cutting depth,which easily produces high residual stress.The residual stress should be analyzed under this particular condition.(2)Multiple factors(e.g.,eccentric swing milling parameters,lubrication conditions,tools,tool and workpiece deformation,and size effect)should be consid-ered comprehensively when modeling instantaneous milling forces,especially for micro milling and complex surface machining.(3)The database of milling force model,including the corresponding workpiece materials,working condi-tion,cutting tools(geometric figures and coatings),and other parameters,should be established.(4)The effect of chatter on the prediction accuracy of milling force cannot be ignored in thin-walled workpiece milling.(5)The cutting force of aviation aluminum alloy milling under the condition of minimum quantity lubrication(mql)and nanofluid mql should be predicted. 相似文献
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