首页> 外文OA文献 >Contributions to understanding the high speed machining effects on aeronautic part surface integrity
【2h】

Contributions to understanding the high speed machining effects on aeronautic part surface integrity

机译:有助于理解高速加工对航空零件表面完整性的影响

摘要

To remain competitive, the aeronautic industry has increasing requirements for mechanical components and parts with high functional performance and longer in-service life. The improvement of the in-service life of components can be achieved by mastering and optimizing the surface integrity of the manufactured parts. Thus, the present study attempted to investigate, experimentally and theoretically, the tool/work material interactions on part surface integrity during the machining of aluminium alloys and hardened materials (low alloy steels) using orthogonal machining tests data. The studied materials are two aluminum alloys (6061-T6 and 7075-T651) and AISI 4340 steel. The AISI 4340 steel was machined after been induction heat treated to 58-60 HRC. These materials were selected in an attempt to provide a comprehensive study for the machining of metals with different behaviours (ductile and hard material).ududThe proposed approach is built on three steps. First, we proposed a design of experiment (DOE) to analyse, experimentally, the chip formation and the resulting surface integrity during the high speed machining under dry condition. The orthogonal cutting mode, adopted in these experiments, allowed to explore, theoretically, the effects of technological (cutting speed and feed) and physical (cutting forces, temperature, shear angle, friction angle, and length Contact tool/chip) parameters on the chip formation mechanisms and the machined surface characteristics (residual stress, plastic deformation, phase transformation, etc.). The cutting conditions were chosen while maintaining a central composite design (CCD) with two factors (cutting speed and feed per revolution).ududFor the aluminum 7075-T651, the results showed that the formation of BUE and the interaction between the tool edge and the iron-rich intermetallic particles are the main causes of the machined surface damage. The BUE formation increases with the cutting feed while the increase of the cutting speed reduces it and promotes the BUL formation on the rake face of the cutting tool. We demonstrated also that by controlling the cutting speed and feed, it is possible to generate a benchmark residual stress state and good surface finish which can improve the in-service life of structural parts made of AA7075-T651aluminum alloys. In this context, correlations have been established between the stress state and the cutting parameters such as cutting forces, shear angle and friction angle.ududWe also investigated the effects of cutting conditions on surface integrity of induction hardened AISI 4340 steel (58-60 HRC) using mixed ceramic inserts. This investigation was motivated by the fact that excessive induction hardening treatment resulted in deep hardened layers (2 mm) with related low compressive residual stresses which may affect the performance of the induction heat treated parts. A judicious selection of the finishing process that eventually follows the surface treatment may overcome this inconvenient. The results showed that the machining process induces significant compressive residual stresses at and below the machined surface. The residual stress distribution is affected by the cutting feed and the cutting speed. On one hand, surface residual stress tends to become tensile when the cutting speed is increased. On the other hand, an increase in cutting feed accentuates surface damage whilst it increases compressive surface residual stress. Microstructural analysis shows the formation of a thin white layer less than 2 μm and severe plastic déformations beneath the machined surface. These results attest that the dry hard machining using ceramic tools may be an alternative to grinding, considered expensive and time consuming, since an enhanced surface integrity in terms of residual stresses and microstructure conditions can be achieved.ududThe first step of this study (experimental study) showed that the surface integrity is closely related to the mechanisms of chip formation. These mechanisms, which are the origin of thermo-mechanical loads, can be quantified by two main parameters: the cutting forces and temperatures generated during machining. Therefore, any attempt to predict the characteristics of the machined surface integrity (residual stresses, transformation phase, etc.), should be, necessarily, involve the prediction of cutting forces and temperature generated during the machining. In this study, we opt out to develop a model for predicting cutting forces and temperatures based on a constitutive equation of the work material that takes into account the effect of strain, strain rate, and temperature. Therefore, the second step of this approach has focused on the identification of the Marusich constitutive equation in order to model the behavior of the materials in high-speed machining. To do so, we proposed an original methodology for identifying the coefficients of Marusich’s constitutive equation (MCE) which demonstrated a good capability for the simulation of the material behaviour in high speed machining. The proposed approach, which is based on an analytical inverse method together with dynamic tests, was applied to aluminums 6061-T6 and 7075-T651, and induction hardened AISI 4340 steel (60HRC). The analytical method consists of determining the material constants inversely using machining tests combined with the response surface models established in the part one of the present thesis. In this section, we investigated the sensitivity of the material constants to the selected temperature models used in the inverse method. Two sets of material coefficients, for each work material, were determined using two different temperature models (Oxley and Loewen-Shaw). The obtained constitutive equations were validated using dynamic tests and finite element (FE) simulation of high speed machining. A sensitivity analysis revealed that the selected temperature model used in the analytical inverse method affected significantly the identified material constants and thereafter predicted dynamic response and machining modeling. In general, material constants obtained using Oxley temperature model gave satisfactory results, compared to Loewen and Shaw model, in predicting the dynamic behaviour and also in predicting the cutting forces during the finite element simulation of the high speed machining of the tested materials.ududFinally, the material models which were identified in the previous step were thereafter implemented in a developed analytical model for predicting cutting forces and températures (the third step of the approach). We tested only the coefficients obtained by the Oxley temperature model, due to their better performance in predicting the cutting forces in FEM compared to those obtained by model Loewen and Shaw ones. This part of the study aimed to verify the coefficients determined for materials and also to generalize the Oxley machining theory for high speed machining of aluminum and hard steel alloy using semi-sharp and honed cutting tool edges. The predicted results were compared with experimental data from the present study and from the literature, covering a large range of cutting conditions (speed, feed, and rake angle). An encouraging good agreement has been found between predicted and measured cutting forces for all tested materials. The strain rate constants in the primary and secondary shear zone were found to be sensitive to the cutting conditions and their effects on the predicted data were discussed in detail. Thanks to the Marusich’s constitutive equation, the Oxley’s machining theory was extended to the high speed machining of aeronautic aluminum alloys and induction hardened steels. The proposed predictive model can be extended also to the prediction of the residual stresses whose their prediction using finite element method is complex and time consuming.ududThrough this experimental and theoretical study, we were able to emphasize the physical mechanisms that govern the chip formation and their effects on the machined surface integrity of two classes of metals (ductile and hard). The proposed approaches can be used in the optimization of the cutting conditions in order to control the surface integrity on the machined parts. Furthermore, the results of this study have been validated for feed rates (10 to 50 μm) comparable to the cutting edge radius (5 and 25 μm) used in the experiments. Thus, the developed models (analytical and finite element) can be extended for studying and modeling the conventional machining processes (turning, milling, and drilling) and nonconventional ones such as the micro-machining process.
机译:为了保持竞争力,航空业对功能部件性能较高且使用寿命较长的机械零部件的要求不断提高。通过掌握和优化所制造零件的表面完整性,可以提高组件的使用寿命。因此,本研究尝试使用正交加工测试数据,在实验和理论上研究铝合金和硬化材料(低合金钢)加工过程中零件表面完整性上的工具/工作材料相互作用。研究的材料是两种铝合金(6061-T6和7075-T651)和AISI 4340钢。 AISI 4340钢经过感应热处理至58-60 HRC之后进行了机械加工。选择这些材料的目的是为了全面研究具有不同性能的金属(延性和硬质材料)的加工。 ud ud建议的方法基于三个步骤。首先,我们提出了一种实验设计(DOE),以实验方式分析干燥条件下高速加工过程中的切屑形成和所产生的表面完整性。在这些实验中采用的正交切削模式,从理论上探讨了工艺参数(切削速度和进给)和物理参数(切削力,温度,剪切角,摩擦角和长度接触工具/切屑)的影响。切屑形成机理和加工表面特性(残余应力,塑性变形,相变等)。选择切削条件的同时要保持具有两个因素(切削速度和每转进给量)的中央复合设计(CCD)。 ud ud对于铝7075-T651,结果表明BUE的形成和刀具之间的相互作用边缘和富含铁的金属间化合物颗粒是机加工表面损坏的主要原因。 BUE的形成随切削进给而增加,而切削速度的增加会降低它,并促进切削刀具前刀面上的BUL形成。我们还证明了通过控制切削速度和进给量,可以产生基准残余应力状态和良好的表面光洁度,从而可以改善由AA7075-T651铝合金制成的结构零件的使用寿命。在这种情况下,应力状态与切削参数(例如切削力,剪切角和摩擦角)之间建立了相关性。 ud ud我们还研究了切削条件对感应淬火AISI 4340钢(58- 60 HRC)使用混合陶瓷插件。这项研究的动机是,过度的感应淬火处理会导致深的硬化层(2毫米),而相关的低压缩残余应力可能会影响感应热处理零件的性能。明智地选择最终在表面处理之后进行的精加工工艺可以克服这种不便之处。结果表明,机加工过程在机加工表面及其下方产生明显的压缩残余应力。残余应力分布受切削进给和切削速度的影响。一方面,当切削速度增加时,表面残余应力趋向于张拉。另一方面,切削进给量的增加加剧了表面损伤,同时增加了压缩表面残余应力。显微组织分析表明,形成了小于2μm的白色薄层,并且在加工表面下方形成了严重的塑性变形。这些结果证明,使用陶瓷工具进行干硬加工可以替代磨削,被认为是昂贵且费时的,因为可以实现在残余应力和微观结构条件方面增强的表面完整性。 ud ud本研究的第一步(实验研究)表明,表面完整性与切屑形成机理密切相关。这些机制是热机械负载的起源,可以通过两个主要参数来量化:切削力和加工过程中产生的温度。因此,任何预测加工表面完整性特征(残余应力,相变相位等)的尝试都必然涉及对切削力和在加工过程中产生的温度的预测。在这项研究中,我们选择基于工作材料的本构方程,开发一种预测切削力和温度的模型,该方程考虑了应变,应变率和温度的影响。因此,此方法的第二步集中在Marusich本构方程的识别上,以便对高速加工中材料的行为进行建模。这样做,我们提出了一种用于识别Marusich本构方程(MCE)系数的原始方法论,该方法论证明了在高速加工中模拟材料行为的良好能力。所提出的方法基于分析逆方法和动态测试,被应用于铝6061-T6和7075-T651以及感应淬火的AISI 4340钢(60HRC)。该分析方法包括使用机械加工测试与本论文第一部分中建立的响应面模型相逆地确定材料常数。在本节中,我们研究了材料常数对逆方法中使用的选定温度模型的敏感性。使用两种不同的温度模型(Oxley和Loewen-Shaw)确定每种工作材料的两组材料系数。使用动态测试和高速加工的有限元(FE)仿真验证了所获得的本构方程。敏感性分析表明,在逆分析方法中使用的选定温度模型会显着影响所识别的材料常数,进而影响动态响应和加工建模的预测。通常,与Loewen和Shaw模型相比,使用Oxley温度模型获得的材料常数在预测动态性能以及在对测试材料进行高速加工的有限元模拟过程中的切削力方面给出了令人满意的结果。最后,在先前步骤中确定的材料模型随后在已开发的分析模型中实施,用于预测切削力和温度(方法的第三步)。我们只测试了通过Oxley温度模型获得的系数,因为与用Loewen和Shaw模型获得的系数相比,它们在FEM中预测切削力方面的性能更好。本部分研究旨在验证确定的材料系数,并推广使用半锐化和珩磨切削刃对铝和硬钢合金进行高速加工的Oxley加工理论。将预测结果与本研究和文献中的实验数据进行比较,这些数据涵盖了大范围的切削条件(速度,进给和前角)。在所有测试材料的预测和测量切削力之间都发现了令人鼓舞的良好协议。发现第一和第二剪切区的应变速率常数对切削条件敏感,并详细讨论了它们对预测数据的影响。由于Marusich的本构方程,Oxley的加工理论扩展到了航空铝合金和感应淬火钢的高速加工。所提出的预测模型也可以扩展到残余应力的预测,其残余应力的有限元预测是复杂且费时的。 ud ud通过这项实验和理论研究,我们能够强调控制切屑的物理机制。的形成及其对两类金属(延性和硬质)的机械加工表面完整性的影响。所提出的方法可用于优化切削条件,以控制加工零件的表面完整性。此外,该研究的结果已经得到了与实验中使用的切削刃半径(5和25μm)相当的进给速度(10至50μm)的验证。因此,可以扩展已开发的模型(分析和有限元),以研究和建模常规的加工过程(车削,铣削和钻孔)和非常规的加工过程(例如微加工过程)。

著录项

  • 作者

    Jomaa Walid;

  • 作者单位
  • 年度 2015
  • 总页数
  • 原文格式 PDF
  • 正文语种 en
  • 中图分类

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号