喷丸强化处理的基本度量方法研究

介绍了喷丸强化度量的基本概念，探讨了喷丸强度标准，研究了度量喷丸强度的“弧高值－时间”关系曲线以及喷丸强度、喷击弹速和弹流密度三者之间的关系，为喷丸加工过程的工艺控制提供了理论依据。     

喷丸齿轮弹流润滑特性分析

利用有限元软件Abaqus仿真得到喷丸强化后齿轮表面形貌,采用MATLAB分析喷丸强化后表面微观形貌对齿轮弹流润滑性能的影响,并与机加工表面的弹流润滑性能进行比较。结果表明：喷丸强化后齿轮的弹流润滑特性总体和机加工齿面保持一致,但喷丸处理后减少了粗糙峰对压力和膜厚的影响,齿面更容易建立起油膜,润滑状态较好;喷丸强化形成的橘皮凹坑有利于储存润滑油剂,齿轮的润滑性能得到了提高。     

齿轮全齿喷丸后弹流润滑特性分析

利用有限元软件Abaqus仿真得到喷丸强化后齿轮表面形貌,采用MATLAB分析喷丸强化后表面微观形貌对齿轮弹流润滑性能的影响,并与机加工表面的弹流润滑性能进行比较。结果表明:喷丸强化后齿轮的弹流润滑特性总体和机加工齿面保持一致,但喷丸处理后减少了粗糙峰对压力和膜厚的影响,齿面更容易建立起油膜,润滑状态较好;喷丸强化形成的橘皮凹坑有利于储存润滑油剂,齿轮的润滑性能得到了提高。     

喷丸强化工艺的喷丸强度测试与分析

对喷丸强化工艺设计时涉及的关键技术指标喷丸强度进行研究。根据喷丸强度测量所需的硬件条件及技术参数,详细阐述了饱和度曲线的绘制方法,对喷丸强度的概念、弧高度值的提取以及影响喷丸强度的因素进行分析,并且对喷丸强化处理时涉及的喷丸强度问题提出了解决方案。     

基于FEM-DEM的粗糙表面喷丸数值模拟与试验研究

考虑试件喷丸前粗糙度的影响,提出了粗糙表面喷丸的有限元与离散元(FEM-DEM)耦合模型.制备喷丸与未喷丸两类45#钢试件,测量了试件喷丸前后表面与亚表面的残余应力.根据测量结果验证耦合模型,研究了喷丸工艺参数对试件亚表面残余应力的影响规律.结果表明,提高表面覆盖率和喷丸强度,均可增大残余压应力峰值,其中,喷丸强度的影...     

喷丸强化对CF53钢摩擦磨损性能的影响

采用3种喷丸强度(0.326,0.401,0.438 mm)对CF53钢进行表面喷丸强化,并在油润滑条件下进行销-盘式摩擦磨损试验,对比研究了喷丸前后试样的表面形貌、显微组织、显微硬度和耐磨性能.结果表明:喷丸强化后试样表面呈现酒窝状凹坑形貌,表面粗糙度、显微硬度和硬化影响区深度随喷丸强度的增加而增大;3种强度喷丸强化...     

喷丸强化工艺覆盖率影响因素和视觉检查

分析了影响喷丸强度覆盖率数据的因素,研究了对于时间变量而言的覆盖率作为概率应变量的演变,讨论了覆盖率和提高零件寿命周期之间的关系,并对复杂几何形状零件喷丸加工提出设计原则。     

基于新型试验装置的TC_4钛合金面接触微动磨损行为研究

自主设计了一套微动磨损夹具装置,可以更好地实现线/面、面/面接触。设置一组喷丸强度梯度处理Ti-6Al-4V合金试样,并与未喷丸磨光态试样进行对比试验分析。探讨喷丸处理对Ti-6Al-4V合金试样面/面接触形式微动磨损性能改善效果。试验结果表明,喷丸强化影响效果随喷丸强度参数变化而波动,其中,0. 20mmA喷丸强度处理在所有喷丸参数中表现最优。微动参数倾向于大滑移状态时,0. 20mmA喷丸强度处理试样较未喷丸磨光试样表现出一定的抗面/面接触形式微动磨损性能;在微动参数倾向于黏着状态时,0. 20mmA喷丸强度处理试样并未表现出良好的微动磨损抗性。     

吹砂对已喷丸Almen A型试片强度及粗糙度的影响

飞机起落架喷丸强化使用的Almen A型试片,在表面处理前需对其进行吹砂处理,用于去除其表面的油污、氧化皮等多余物,而吹砂是否会影响已喷丸过的Almen A型试片的喷丸强度值及粗糙度值,且这种影响是否符合PCS2300及PCS2610规范的要求。为了掌握吹砂对已喷丸过的Almen A型试片的喷丸强度及粗糙度的影响,对吹砂对Almen A型试片的喷丸强度及表面粗糙度的影响进行了试验研究。通过对符合SAE J442标准的Almen A型试片进行喷丸强化及喷丸强化+吹砂处理,通过对比分析法,从而得出吹砂对Almen A型试片喷丸强度及粗糙度的影响。通过试验研究发现,吹砂有利于降低喷丸后的Almen A型试片的表面粗糙度值和喷丸强度值;根据试验结果可知,喷丸后的Almen A型试片经过吹砂后,其表面粗糙度值小于Ra3.2μm,其喷丸强度值减小量不大于原值的10%,符合PCS2300及PCS2610规范的要求。     

喷丸强化对新型7055-T7751铝合金疲劳性能的影响

对7055-T7751新型铝合金表面进行了陶瓷丸喷丸强化处理,采用X射线衍射仪、表面轮廓仪、扫描电子显微镜、显微硬度计等研究了喷丸强度、喷丸覆盖率等工艺参数对铝合金表面残余应力场、表面粗糙度、表面损伤及表面加工硬化和疲劳性能的影响。结果表明:优化工艺参数下的喷丸强化能够显著提高该铝合金的疲劳性能,并不是喷丸强度或喷丸覆盖率越高强化效果越好,而是存在合理的喷丸强化参数范围,在优化条件下铝合金可以获得良好的综合表面完整性,疲劳断裂抗力最高;确定的优喷丸参数为喷丸强度0.15mm,覆盖率100%,以此参数强化处理的7055-T7751铝合金的疲劳寿命是基材的2.7倍。     

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.