6061-T651铝合金单颗磨粒磨削仿真

通过简化并建立单颗磨粒磨削模型,采用ANSYS LS-DYNA进行对6061-T651特种铝合金磨削过程的理论研究和仿真分析,总结了单颗磨粒的磨削速度、磨削深度等工艺参数对磨削力大小以及磨屑的影响。研究表明:随着磨削速度的增加,单个磨料颗粒的磨削力减小,并且递减速率呈先增大后减小的趋势;而磨削深度的增加则会使单个磨料颗粒的磨削力增大,且递增速率逐渐减缓。磨削过程中,磨屑形状受加工参数的影响,其中,磨削深度对磨屑形状的影响比磨削速度对磨屑形状的影响更大。     

AA7075板材热处理的增塑机制及成形性能

结合生产工艺过程，研究了成形所需固溶处理、工序衔接所需自然时效、性能恢复所需人工时效对板材力学性能和成形性能的影响；通过金相显微镜、扫描电子显微镜和能谱分析等手段，探索热处理对板材显微组织与宏观力学性能的影响。结果表明：AA7075板材经固溶(480 ℃,0.5 h)水淬且自然时效处理后，最大力总伸长率提高85%、屈服强度降低60%，后经人工时效(120 ℃,12 h)处理，板材可完全恢复力学性能；固溶后,板材成形极限大幅提高，回弹比率显著减小；后继时效处理对弯曲角变化影响微弱。     

6061-T651铝合金动态力学性能及J-C本构模型的修正

为合理描述6061-T651铝合金的应力流动行为,利用万能材料试验机和霍普金森压杆,分别进行准静态、高温和高应变率下的材料力学性能测试,获得材料在不同条件下的应力应变曲线。基于试验结果,修正Johnson-Cook本构模型得到MJC(Modified Johnson-Cook)模型,并标定MJC模型各项参数。为校验MJC模型及参数的有效性,利用一级气炮发射直径为5.95mm的圆柱弹体冲击刚性靶的Taylor杆试验以及直径为12.68mm的刚性弹撞击厚度为2mm靶板的试验。最后,采用ABAQUS/Explicit有限元软件建立Taylor杆和弹靶冲击试验的三维模型,基于MJC本构模型进行Taylor杆冲击、以及结合MMC(ModifiedMohr-Coulomb)断裂准则进行弹靶冲击的数值模拟计算。研究结果表明,修正的MJC本构模型能够有效地描述6061-T651铝合金材料在大应变、高应变率和高温下材料的应力流动行为和变形行为。     

高速侧铣参数对7050-T7451铝合金表面粗糙度的影响

为提高航空结构件加工效率和表面质量,通过单一铣削参数实验,研究采用两种硬质合金刀具在高速铣削7050-T7451铝合金时,主轴转速、径向铣削深度、铣削进给速度等切削参数以及加工方式(顺铣、逆铣)对表面粗糙度的影响.分析表明:表面粗糙度随刀具尺寸和径向切深增大而增加,在铣削进给速度增加趋势下仅有较小波动,不受主轴转速直接...     

MEMS based acoustic thermomechanical characterization of aluminum 6061-T651 beams

Temperature-based testing is an important tool in determining the mechanical characteristics of structures. Metallic structures, such as aluminum beams, respond to temperature variations. Similarly, Young’s modulus of elasticity of the material has a temperature dependence that contributes significantly to the overall mechanical qualities of the material. In this work, a method based on flexural frequency response is described in which the variation in the experimental 5th natural frequency under thermal loading is employed to extract the coefficient of thermal dependence of Young’s modulus. This coefficient is then employed in the theoretical model to validate the experimental 2nd, 3rd, 4th and 5th natural frequencies of the aluminum beam. A micro-electro-mechanical-systems based microphone is used to monitor the frequency response of the beam. Constant geometry and constant elasticity models are presented and compared. The proposed method is applied to an aluminum 6061-T651 beam. Experimental results are in good agreement with the theory.     

On the application of a micromechanical small fatigue crack growth model to predict fretting fatigue life in AA7075-T6 under spherical contact

This work presents a method for assessing the fretting fatigue life by estimating the fatigue crack growth rate from the regime of microcracks to the final failure, which is achieved using a two-threshold small fatigue crack growth model. The propagation thresholds are associated with the interaction of the "monotonic plastic zone" and the "cyclic plastic zone" with the microstructure of the material. The predicted fatigue life and the estimated non-propagating cracks agree very well with the experimental fretting fatigue tests with spherical contact in 7075-T6 aluminium alloy.     

7075T651铝合金板材内部初始残余应力分布研究

针对材料内部残余应力分布的传统剥层测量方法,对底部贴片的剥层法进行改进,通过测量底部释放的应变,结合有限元方法模拟残余应力释放过程中得到的各剥除层的应变释放系数,计算出了剥除层释放的残余应力。运用弹性力学理论推导得到了材料内部初始残余应力的修正公式。随后基于两种方法对典型7075T651航空铝合金预拉伸板的内部残余应力进行了测量,并对测量结果进行了分析和比较。结果表明,改进法能够有效评估材料内部初始残余应力分布规律,但是在个别深度处测量精度有待进一步提高。     

Effects of overlapping formed via pin-offsetting on friction stir weldability of AA7075-T651 aluminum alloy

Journal of Mechanical Science and Technology - In this study, AA7075-T651 aluminum alloy was joined by friction stir welding (FSW) method, using two different pin offset values, and the...     

Fretting fatigue behavior of Al7075-T6 at sub-zero temperature

In some fretting fatigue applications, such as aero industry, the temperature may drop well below −50 °C Fretting fatigue behavior of aluminum alloy Al7075-T6 is investigated at temperatures of 24, 0, −25 and −50 °C in this work. The results show that (i) normal fatigue life increases considerably at sub-zero temperatures up to around 85% for low working stresses and reduces to about 40% for higher working stresses; (ii) fretting fatigue life at sub-zero temperatures rises significantly up to around 220% for low working stresses and reduces to about 50% for higher working stresses; (iii) ultimate strength of material changes from −15% to 15% under the fretting fatigue test conditions; and finally (iv) some parameters such as mechanical properties and fatigue behavior of material at low temperatures, contact load relaxation, crack closure, oxidation and some unknown sources can be thought to be responsible for fretting fatigue behavior of Al7075-T6 at sub-zero temperatures.     

硬态切削高强度钢表面完整性的研究

高强度钢45CrNiMoVA以其良好的力学性能,被广泛作为车辆悬挂系统弹性零件扭杆的材料。45CrNiMoVA是典型的高强度钢,属于难加工材料,扭杆在实际应用中通常经常承受大应力、应变、冲击影响,疲劳寿命成为影响其断裂失效的重要参数。表面质量能够影响材料的疲劳强度、磨损率、耐腐蚀性等特征。硬态切削可以有助于在简化加工工艺的同时,达到预期的表面质量。对于已知的各种参数,如切削速度、进给率和切削深度对表面完整性都有很大的影响。在本试验中,表面完整性主要通过表面粗糙度、残余应力、微观硬度等方面进行分析。     

低温切削7075铝合金鳞刺形成规律及抑制措施

针对干切削铝合金工件表面易产生鳞刺、表面完整性较差的问题,采用液氮冷却方式在不同切削参数下对7075铝合金进行了正交切削试验,使用扫描电子显微镜和3D光学轮廓仪分别表征了已加工表面形貌、鳞刺分布和鳞刺尺寸,分析了切削速度、进给量、刀具前角和冷却方式(干切削、液氮冷却、切削液)对已加工表面鳞刺分布和尺寸的影响,并基于鳞刺...     

An Investigation into the Effect of Normal Load Frequency on Fretting Fatigue Behavior of Al7075-T6

Most previous studies on fretting fatigue have been accomplished under constant normal loading and less attention has been paid to cyclic normal loading. An innovative test apparatus was specially designed and manufactured for fretting fatigue tests under cyclic loading in this work and the fretting fatigue behavior of Al7075-T6 was investigated at different normal load frequencies. A finite element model was developed to study the effect of normal load frequency on the contact stress distribution. It was found that the cyclic normal load has a more damaging effect on fretting fatigue life compared to constant normal load, particularly at lower frequencies. The results showed that at the normal load frequency of f = 1 Hz, fatigue life decreased by 52% in the high cycle fatigue regime and 28% in the low cycle fatigue regime. The experimental results also indicated that at the normal load frequency of 80 Hz, the fretting fatigue life converged to its corresponding life under constant normal load condition. The fracture surface and the fretting area of the specimens were examined using both optical and scanning electron microscopy (SEM). The experimental observations showed that the dominant partial slip condition with a wider slip region compared to constant normal loading, severe delamination, and higher oxidation rate due to the normal load release at each cycle, are the most important reasons for significant reductions in fretting fatigue life, under cyclic normal loading, especially for low normal load frequencies.     

AA7075-T6圆筒形零件热态颗粒介质压力成形过程的力学分析

基于颗粒介质传压性能试验和AA7075-T6板材材料性能试验,对采用热态颗粒介质压力成形(HGMF)工艺拉深成形圆筒形件的法兰区、传力区和自由变形区进行了塑性力学分析,求解得到内压非均匀分布条件下成形压力的函数关系式,并与实测数据进行比对。分析结果表明,在成形中后期产生较大的偏差,理论求解最大成形力低于实测值24.6%。工艺试验研究表明,在成形温度为250℃条件下,采用HGMF工艺可一道次成形AA7075-T6圆筒形零件(底部为自由变形区)的极限拉伸比(LDR)为1.71。HGMF工艺操作便捷,装置简单,可在通用压力设备上实现轻合金板材件热成形,适用于航空、航天和军工等领域中小批量产品。     

高速铣削7050-T7451铝合金表面粗糙度研究

高速铣削广泛用于航空铝合金材料的加工,以7050-T7451铝合金材料为试验对象,运用正交试验方法分析研究了铣削该铝合金材料时,切削速度、切削深度、切削宽度和每齿进给量4个因素对表面粗糙度的影响规律,并通过多元非线性回归分析得出表面粗糙度的经验公式.研究结果表明:加工表面呈交叉织网状形貌,表面粗糙度随每齿进给量和铣削深度的增大而增大,随切削速度的增大而减小,切宽对铝合金表面粗糙度的影响不明显.铣削参数对表面粗糙度的影响显著性依次为:每齿进给量fz切削速度v轴向切削深度ap径向切削宽度ae.     

Optimization of end mill tool geometry parameters for Al7075-T6 machining operations based on vibration amplitude by response surface methodology

This paper aims at developing a statistical model to envisage vibration amplitude in terms of geometrical parameters such as radial rake angle, nose radius of cutting tool and machining parameters such as cutting speed, cutting feed and axial depth of cut. Experiments were conducted through response surface methodology experimental design. The material chosen is Aluminum (Al 7075-T6) and the tool used was high speed steel end mill cutter with different tool geometry. Two channels piezoelectric accelerometers were used to measure the vibration amplitude. The second order mathematical model in terms of machining parameters was built up to predict the vibration amplitude and ANOVA was used to verify the competency of the model. Further investigation on the direct and interactive effect of the process parameter with vibration amplitude was carried out for the selection of process parameter so that the vibration amplitude was maintained at the minimum which ensures the stability of end milling process. The optimum values obtained from end milling process are Radial rake angle-12°, Nose radius-0.8 mm, Cutting speed-115 m/min, Cutting feed rate-0.04 mm/tooth, axial depth of cut-2.5 mm. The vibration amplitude exhibited negative relationship with radial rake angle and nose radius. The dominant factors on the vibration amplitude are feed rate and depth of cut. Thus it is envisaged that the predictive models in this study could produce values of the vibration amplitude close to the experimental readings with a 95% confidence interval.     

铝合金高速切削表面粗糙度影响因素研究

为有效降低高速切削中铝合金的表面粗糙度值,通过多因素正交试验和单因素试验对各铣削参数进行研究,结果显示:各参数对铝合金表面粗糙度影响程度从大到小的顺序是:切削深度、主轴转速、每齿进给量、行距,且转速为18000r/min,每齿进给量为0.075mm,行距和每齿进给量一致,选择较小的切削深度时,在铝合金表面可获得较好的加工质量。     

Modification of fretting fatigue behavior of AL7075-T6 alloy by the application of titanium coating using IBED technique and shot peening

In this work, improvement in fretting fatigue life of AL7075-T6 has been investigated by titanium surface coating using ion-beam-enhanced deposition (IBED) technique and shot peening. From the experiments, the following conclusions were derived: (i) Shot peening increased the fretting fatigue life up to 350%. (ii) Titanium coating increased the fatigue life up to 100% with respect to virgin specimens for low working stresses, while it reduced the fatigue life at higher working stresses significantly. (iii) Titanium coating+shot peening increased the fatigue life up to 130% with respect to the virgin specimens for low working stresses, while it reduced the fatigue life at higher working stresses significantly. The highest and the lowest increase in coefficient of friction are obtained for virgin and shot-peened+titanium-coated specimens, respectively. IBED surface-modification technique is not successful in reducing fretting fatigue, except at low stresses.     

7075铝合金阳极氧化膜腐蚀性能研究

本文以7075铝合金为研究对象,采用硫酸直流电阳极氧化法制备氧化膜,并通过正交试验研究了合金在铜加速乙酸盐雾腐蚀条件下的腐蚀性能。由极差分析可知:在盐雾腐蚀条件下,时间是最大的影响因素,其次是温度对合金的影响,最小的是腐蚀液浓度。阳极氧化后的合金主要以点蚀为主,在72 h、35℃、3%腐蚀液浓度条件下,蚀坑最深值可达112.6μm,阳极氧化对均匀腐蚀的改善作用明显大于点腐蚀。     

曲面铝合金锤击平整技术研究

以曲面铝合金为例,利用工业机器人锤击的方式对曲面类零件表面进行平整,并探究各锤击工艺参数对其表面的粗糙度、硬度及表面形貌的影响.将锤击装置装夹到工业机器人上,控制工业机器人以矩形光栅式运动路径对曲面铝合金表面进行锤击加工,并对锤击后表面的粗糙度、硬度及表面形貌进行测量观察.结果表明:经锤击加工后的铝合金表面粗糙度可达0...     

7075铝合金杯形反挤压成形计算机仿真

基于DEFORM-3D仿真软件,分析了7075铝合金带筋杯形件反挤压成形过程,研究了挤压速度、扭转速度、坯料初始温度对成形过程的影响,通过正交试验获得最佳成形工艺参数,并将传统的挤压成形与扭转挤压成形进行对比。结果表明,在传统反挤压的基础上,扭转作用使得坯料成形所需载荷降低,金属内部等效应变分布更均匀,通过正交试验最终得到了优化后的成形工艺参数,为铝合金杯形件反挤压成形提供理论基础。