40Cr钢低温超塑性的研究

研究了40Cr钢的低温超塑性。结果表明:经3次840℃×40 min水淬+650℃×2h回火的超塑性预处理后,40Cr钢的组织为回火索氏体,晶粒尺寸为5-10μm,在温度为650℃、初始应变速率为3.16×10-4 s-1的拉伸变形条件下,流变应力为:108.1 MPa,断后伸长率为254％,应变速率敏感性指数m值为0.221,超塑变形的主要机制可描述为原子扩散控制的晶界滑动。     

晶粒尺寸对TC4钛合金超塑性行为及变形机理的影响

研究了不同晶粒尺寸(2,8,18μm)T℃4钛合金在温度860～950℃和应变速率5×10-4～5×10-3S-1条件下的超塑性拉伸变形行为及组织演变,分析了晶粒尺寸对该合金超塑性变形行为及变形机理的影响.结果表明:在温度890℃、应变速率5×10-4S-1的变形条件下,细晶(2μm)合金超塑性变形的断后伸长率高达1 300%,而粗晶(18μm)合金的仅为450%;细晶(2～8μm)A金超塑性变形后,平均应变速率敏感指数m值在0.50左右,晶粒保持较好的等轴状,在α/α仅晶界、α晶内均未观察到明显的位错,在α/β晶界附近发现少量的位错;粗晶(18 μm)合金超塑性变形后,m值仅为0.30,晶粒等轴程度下降,在α/α晶界及α晶内均发现大量位错,且在α晶内发现亚晶.     

轧制工艺参数对ZK60镁合金组织和拉伸性能的影响

在不同变形温度(275~350℃)和应变速率(5~25s~(-1))下,采用单道次大变形量(80%)轧制ZK60镁合金,研究了变形温度和应变速率对合金显微组织和拉伸性能的影响。结果表明:随着变形温度的升高和应变速率的增大,合金的再结晶体积分数增加;当变形温度不高于300℃时,随着应变速率的增大,再结晶晶粒尺寸先减小后增大,抗拉强度先增后降,伸长率增大;而当温度高于300℃时,再结晶晶粒尺寸先增大后减小再增大,抗拉强度先降低后增大再降低,伸长率增大;在温度300℃,应变速率10s~(-1)下轧制后,所得ZK60镁合金板的拉伸性能最好,抗拉强度和伸长率分别为358 MPa,21.5%。     

铸态铝黄铜的超塑性

本文 研究了未经任何预处理的大晶粒铸态铝黄铜（ZHA166-6-3-2）的超塑性,结果表明：在变形温度为520～585℃,初始应变速率为2.6×10-4～6.6×10-3s-1范围内,超塑拉伸的伸长率可达到120%以上,最佳应变速率为2.6×10-3s-1,变形温度为575℃,最大伸长率为230%,应变速率敏感性指数为0.32,金相组织分析表明：超薄变形主要发生在大晶粒内部,超塑变形促进亚晶的形成和动态再结晶的进行。     

93WNiFe合金的高温变形机制

用Instron1195试验机研究了93WNiFe合金在温度10～900℃,应变速率6.67×10-4～6.67×10-2s-1的动态拉伸性能。结果表明:93WNiFe合金流变应力随温度的升高而降低,随应变速率的升高而增加;合金的变形激活能Q和应力指数n明显分为10～300℃、400～600℃和700～900℃三个温度阶段,93WNiFe合金在设定的试验温度范围内存在三个不同的变形机制。     

AZ61镁合金加工图及其在轧制成形中的应用

采用Gleeble-1500型热模拟试验机对AZ61镁合金在变形温度250~400℃、应变速率0.001~10 s-1条件下进行热压缩试验,研究了合金的热压缩变形行为,得到了其加工图,并将得到的最佳变形工艺成功应用于轧制成形。结果表明:合金在变形温度250~400℃、应变速率10 s-1的变形条件下具有较高的能量耗散效率,该工艺参数范围为合金的最佳变形工艺;在该工艺参数范围内进行轧制变形可获得组织均匀、力学性能优异的镁合金板材,其平均晶粒尺寸在3~10μm之间,抗拉强度和伸长率则分别在292.9~329.7 MPa和21.4%~27.5%之间。     

Al-6.3Cu-0.29Mn(S147)合金形变热处理和组织结构对其超塑性的影响

本文对Al-6.3Cu-0.29 Mn 合金的形变热处理、超塑性变形力学行为、显微组织、空洞及断裂等进行了研究。形变热处理可使耐热的Al-6.3Cu-0.29 Mn 合金的晶粒细化到9微米以下。合金在500℃以(?)=3.3×10~(-4)s~(-1)应变速率拉伸可呈现超塑性,延伸率达365%,流动应力为1.2MPa,m=0.76。第二相粒子的硬度、尺寸和分布是重要参数。小尺寸粒子对晶界有钉扎作用,可防止晶粒长大,大而硬的不易变形的粒子在变形中可能抑制晶界滑动,并因空洞而使试样早期断裂。     

SiCp/LD2铝基复合材料的超塑性

对搅拌铸造、小挤压、热轧和冷轧制备的15%SiCp/LD2铝基复合材料的超塑性进行了研究.研究表明在温度为833K、初始应变速率为8.9×10-4s-1的拉伸变形条件下,其伸长率为250%;适量液相对该复合材料的超塑性具有关键作用.     

水淬调质态40Cr钢超塑性的研究

研究了 40Cr钢经水冷淬火和高温回火后的超塑性。结果表明 :40Cr钢的晶粒尺寸为 1 0～ 1 5 μm ,在温度为 75 0℃、初始应变速率为 1 0×1 0 - 3s- 1 的拉伸变形条件下 ,超塑伸长率为 30 4 % ,流变应力为 63 0MPa ,应变速率敏感性指数m值为 0 2 2 7,超塑性变形的机制可描述为原子扩散控制的晶界滑动。     

高应变速率条件下1200MPa级冷轧双相钢塑性变形微观机理的研究

通过在CMT4105试验机上进行准静态拉伸试验,在Hopkinson拉杆试验机上进行动态拉伸试验。在常温下,对DP1200冷轧双相钢进行应变速率为1×10~(-4) s~(-1)、1×10~(-3) s~(-1)、1×10~(-2) s~(-1)的准静态拉伸试验,以及应变速率为500 s-1、1 000 s-1、2 250 s-1的动态拉伸试验,并对拉伸断口进行形貌分析。结果表明:DP1200冷轧双相钢在准静态和动态变形条件下,随应变速率的增大,屈服强度s0.2从723 MPa增加到998 MPa,抗拉强度sb从1 205 MPa增加到1 515 MPa,断后伸长率从9.0%下降到7.7%,屈强比从0.60上升到0.66。准静态和动态拉伸的韧断口都呈现窝状,为韧性断口。应变速率为1×10~(-4) s~(-1)、1×10~(-3) s~(-1)、1×10~(-2)s~(-1)、500 s~(-1)、1 000 s~(-1)、2 250 s~(-1)断口韧窝平均尺寸分别为7.5μm、7.2μm、6.9μm、4.3μm、3.5μm和2.6μm,准静态拉伸不同应变速率下韧窝形貌变化不大,动态拉伸条件下随应变速率的增加断口韧窝变深。     

Minimal Realization of Linear Graph Models for Multi-physics Systems

An engineering system may consist of several different types of components,belonging to such physical"domains"as mechanical,electrical,fluid,and thermal.It is t...     

INTEGRAL EQUATION METHOD＇S APPLICATION IN HOLE-EDGE STRESS OF COMPOSITE MATERIAL PLATE WITH DIFFERENT SHAPED HOLES

The strength of composite plate with different hole-shapes is always one of the most important but complicated issues in the application of the composite material. The holes will lead to mutations and discontinuity to the structure. So the hole-edge stress concentration is always a serious phenomenon. And the phenomenon makes the structure strength decrease very quickly to form dangerous weak points. Most partial damage begins from these weak points. According to the complex variable functions theory, the accurate boundary condition of composite plate with different hole-shapes is founded by conformal mapping method to settle the boundary condition problem of complex hole-shapes. Composite plate with commonly hole-shapes in engineering is studied by several complex variable stress fimction. The boundary integral equations are founded based on exact boundary conditions. Then the exact hole-edge stress analytic solution of composite plate with rectangle holes and wing manholes is resolved. Both of offset axis loadings and its influences on the stress concentration coefficient of the hole-edge are discussed. And comparisons of different loads along various offset axis on the hole-edge stress distribution of orthotropic plate with rectangle hole or wing manhole are made. It can be concluded that hole-edge with continuous variable curvatures might help to decrease the stress concentration coefficient; and smaller angle of outer load and fiber can decrease the stress peak value.     

Non-monotonic material contrast in scanning ion and scanning electron images

30 keV Ga⁺ focused ion beam induced secondary electron (iSE) imaging was used to determine the relative contrast between several materials. The iSE signal compared from C, Si, Al, Ti, Cr, Ni, Cu, Mo, Ag, and W metal layers does not decrease with an increase in target atomic number Z₂, and shows a non-monotonic relationship between contrast and Z₂. The non-monotonic relationship is attributed to periodic fluctuations of the stopping power and sputter yield inherent to the ion–solid interactions. In addition, material contrast from electron-induced secondary electron (eSE) and backscattered electron (BSE) images using scanning electron microscopy (SEM) also shows non-monotonic contrast as a function of Z₂, following the periodic behavior of the stopping power for electron–solid interactions. A comparison of the iSE and eSE results shows similar relative contrast between the metal layers, and not complementary contrast as conventionally understood. These similarities in the contrast behavior can be attributed to similarities in the periodic and non-monotonic function defined by incident particle–solid interaction theory.     

Application of Feature Extraction through Convolution Neural Networks and SVM Classifier for Robust Grading of Apples

This paper proposes a novel grading method of apples,in an automated grading device that uses convolutional neural networks to extract the size,color,texture,an...     

分布动态载荷识别的抗噪处理

针对正交多项式频域法在用多种响应对矩形薄板进行载荷识别中抗噪性较差的问题,综合运用平均法、矩阵预处理和奇异值截断法等方法对之进行改善,并引入空间映射的思想,将该方法的应用范围拓展为复杂的模型.利用仿真算例,证实了该方法具有较好的抗噪性.     

基于MELTAC-N平台的核电厂安全级DCS环网研究与测试

针对工程实践中环网通讯相关问题的处理缺乏理论基础及国产化安全级DCS平台的开发缺乏成熟经验借鉴问题,对基于MELTAC-N平台核电厂安全级DCS环网的软硬件实现进行了研究。提出了安全级DCS环网双环网冗余设计、光切换开关设计等硬件设计方法,以及以RPR协议为基础,采用全数据收发策略的软件设计方法。在CPR1000安全级DCS平台上对安全级DCS环网的可靠性及实时性进行了评价,并进行了容错能力、响应时间及响应时间稳定性测试验证实验。结果表明,基于MELTAC-N平台安全级DCS环网软硬件设计具有较好的容错能力及响应时间稳定性。     

Short-Term Relay Quality Prediction Algorithm Based on Long and Short-Term Memory

The fraction defective of semi-finished products is predicted to optimize the process of relay production lines, by which production quality and productivity ar...     

End-to-End Multiview Gesture Recognition for Autonomous Car Parking System

The use of hand gestures can be the most intuitive human-machine interaction medium.The early approaches for hand gesture recognition used device-based methods....     

The laboratory simulation of abrasive wear

Abrasive wear has long been recognised as one of the most potentially serious tribological problems facing the operators of many types of plant and machinery; several industrial surveys have indicated that wear by abrasion can be responsible for more than 50% of unscheduled machine and plant stoppages. Locating the operating point of a tribological contact in an appropriate operational ‚map’︁ can provide a useful guide to the likely nature and origins of the surface degradation experienced in use, though care must be exercised in choosing the most suitable parameters for the axes of the plot. Laboratory testing of materials and simulations of machine contacts are carried out for a number of purposes; at one level for the very practical aims of ranking candidate materials or surface hardening treatments in order of their wear resistance, or in an attempt to predict wear lives under field conditions. More fundamentally, tests may be aimed at elucidating the essential physical mechanisms of surface damage and loss, with the longer term aim of building an analytical and predictive model of the wear process itself. In many cases, component surface damage is brought about by the ingress of hard, particulate matter into machine bearing or sealing clearances. These may be running dry although, more usually, a lubricant or service fluid is present at the interface. A number of standardised wear test geometries and procedures have been established for both two- and three-body wear situations, and these are briefly described. Although abrasive wear is often modelled as following an ‚Archard’︁ equation (i.e. a linear increase in material loss with both load and time, and an inverse dependence on specimen hardness) both industrial experience and laboratory tests of particularly lubricated contacts show that this is not always the case: increasing the hardness differential in an abrasively contaminated lubricated pair may not always reduce the rate of damage to the harder surface.     

ANGULAR DISTORTION ALLOWABLE VALUE AND ASSESS METHOD OF WELD ON COKE TOWER

A graph as the new engineering method for estimate the safety of bulging deformation of coke tower is proposed. Through stresses analysis of circumferential weld of coke tower and comparing the stresses produced by pressure with heat stress of steady state, residual stress, bending stress produced by both itself weight and wind loads, it showed that the stresses produced by pressure on the angle distortion are the main factor of equivalent stress of the combined stress. After comparing four kinds of stress controlling conditions, the relation to stress with depth of angular distortion, grade of curvature of angular distortion and half of region of angular distortion has been inferred. Graph of deformation allowable value of coke tower for different condition by angular distortion and half of region of angular distortion has been plotted. The five steps for its engineering use have been explained. The lighter the grade of curvature is, the larger of bulge allowance, may be, and the bigger of depth of angular distortion may pose too. For the coke tower with a popular structure of Dg 5 400 mm×28 mm, the result by graph is nearly more than the result of two formulas formed by other research, the error is less than 7.0%. But, the graph can be easily applied to different size of angular distortion.