一种镍基单晶超合金高温低周疲劳的晶体取向相关性模型

在950℃t对[001]、[012]、[112]、[011]和[114]晶体取向的镍基单晶超合金DD3试样进行了对称循环低周疲劳(ICF)试验。应变率取1.0×10-2,1.33×10-3,0.33×10-3s-1.试验结果表明,LCF特性显着地取决于晶体取向和应变率。试样断口细观分析表明,除了[001]取向试样外,其余所有试样断口上均有明显的等间距疲劳纹。这些疲劳纹由微裂纹组成,其间距取决于试样的晶体取向和总应变范围。基于晶体滑移理论,建立了疲劳纹间距和总分切应变范围及取向和应变率函数的一个简单关系。对Lall-Chin-Pope(LCP)模型进行修正并推广应用于循环塑性和疲劳寿命研究,提出了一个晶体取向和应变率参数,该参数可以很好地描述镍基单晶超合金高温低周疲劳循环塑性和疲劳寿命的晶体取向和应变率相关性。     

循环载荷下缺口板的弹塑性应变分析——塑性各向异性强化理论的应用

为了估算承受低周疲劳时工程构件的寿命,需要研究缺口件在低周交变负荷时的应变分布.由于循环载荷作用下材料的鲍兴效应不能忽略,需要应用塑性各向异性强化模型.从本文的计算结果与实验结果的比较可以看出即使是线性随动强化模型对解决循环加载下的应变计算还是很有效的.     

描述低周疲劳裂纹扩展速率的循环J积分新参量

探讨了低周疲劳加载条件下的应力增量．应变增量关系，提出了模拟裂纹疲劳扩展的二维模型以建立新的循环．积分参量，详细阐述了该积分参量的定义、主要特点、物理意义以及数值计算方法，并通过紧凑拉伸试样的疲劳试验检验该积分参量的有效性．结果表明：该积分参量能够较好描述恒幅低周疲劳裂纹的扩展速率．此外，基于积分参量体系，从能量的角度解释了疲劳迟滞现象．     

机床疲劳载荷的统计分析和概率设计

本文对复杂的机床传动系统的动力特性和疲劳载荷进行统计分析，对传动件的疲劳寿命也视为概率分布状态，在探讨载荷与疲劳寿命的分布规律基础上，提出了机床传动件概率设计的理论公式，用这种新的设计方法可以预测传动件的可靠度或疲劳寿命。     

焊接接头疲劳寿命预测研究

利用作者构造的焊接接头疲劳抗力起始—扩展模型,可精确预测焊件的疲劳寿命,预测结果与实测结果吻合良好。     

基于LiToSim平台的疲劳寿命评估LtsFatigue软件开发及应用

针对结构的疲劳问题,考虑随机载荷作用,在自主开发的LiToSim平台基础上,嵌入结构疲劳分析数值计算程序。基于LiToSim平台开发LtsFatigue疲劳软件,运用时域疲劳算法,通过雨流计数法对应力时程曲线处理并计算结构疲劳寿命;引入频域疲劳算法,基于应力响应功率谱根据应力循环分布估算疲劳寿命;通过齿轮算例进行疲劳分析,与商业软件对比,验证了LtsFatigue定制化疲劳软件时域法、频域法的计算精度,同时,频域算法有效提高了计算效率,凸显了LtsFatigue软件的优势。基于LiToSim平台的LtsFatigue定制化疲劳软件开发,对大型复杂结构的疲劳仿真具有重要的应用价值。     

TFR、TRV和CE模型序加试验下WEIBULL分布产品的失效分布

本针对TFR模型，首次提出将步加试验推广至序加试验，就两参数Weibull分布给出了损伤因子函数，同时给出了产品寿命的残存函数，另外针对TRV模型，在序加试验下就两参数Weibull分布给出了损伤系数，同时给出了产品寿命的残存函数。     

回转窑滚圈多轴疲劳寿命预测及与轴线偏移关系研究

结合轴线偏移情况开展回转窑滚圈多轴疲劳寿命研究,采用了Wang和Brown提出的多轴疲劳准则和雨流计数法及Miner准则进行累积损伤评估．回转窑运行轴线偏移会导致滚圈承受的支承载荷分布严重不均,因此引入载荷比来描述轴线偏移程度以进一步定量分析滚圈应力．采用有限元软件ANSYS进行了各载荷比下滚圈的接触应力分析,并根据滚动接触区域情况计算得到了切向摩擦应力．以某回转窑滚圈为分析对象,计算得到了随载荷比变化的疲劳寿命曲线,揭示了轴线偏移对滚圈疲劳寿命的影响规律．研究对减少滚圈疲劳失效有重要意义,同时也可作为轴线调整和优化调窑的理论依据．     

机电产品可靠性寿命试验数据的灰色预测方法

采用灰色系统预测理论对产品可靠性寿命试验数据进行预测,提出了建立产品可靠性寿命试验数据的灰色预测NGM(1,1)模型的方法,并通过采用试验数据序列与预测数据序列总体分布函数相等性检验方法确认灰色预测NGM(1,1)模型用于产品可靠性寿命试验数据预测是可行的.算例结果表明,采用灰色预测方法预测产品可靠性寿命试验数据并进行相关的分布函数参数估计有较高的精度,可达到缩短试验时间和节约试验费用目的.     

疲劳断裂非平衡统计理论——(Ⅱ)从微观机理到疲劳断裂的宏观特性

本文给出了微裂纹的随机演化方程,结合位错机理解得了微裂纹密度的分布函数,求出了疲劳断裂几率和可靠性,进而导出了σ_α-N曲线、疲劳寿命的统计分布和统计平均值。     

A Method to Estimate the Inelastic Response in Notched Structures of Anisotropic Materials with Elastic ‐ Perfectly Plastic Behavior

The fatigue strength of engineering structures is often limited by notches which arise from constructive features or manufacturing defects. The constitutive behavior in notch regions is then characterized by small plastic zones which are contained in an elastic region. To avoid costly plastic calculations, approximate methods have been developed to estimate the inelastic stress‐strain response at the notch tip. One of the first and best known approximate models is that of Neuber which, over the last 40 years, has received considerable attention particularly in connection with fatigue life prediction. Numerous studies have been conducted to the verification and the generalization of the Neuber approach which respect to multiaxiality, cyclic loading and creep conditions. Recently an extension of the Neuber method to anisotropic materials has been proposed in [1] and applied to directionally solidified and single crystal Nickel based superalloys as they are used in high temperature material applications. In this short notice we modify the approach in [1] for the special case of an elastic ‐ perfectly plastic anisotropic material.     

Creep and damage accumulation in orthotropic composites under cyclic loading

Experimental results and theoretical prediction of the response of glassfiber-reinforced polyester under quasi-static, static (creep), and cyclic (fatigue) loading are presented. The nonlinear strain component at static loading and the strain amplitude rate at cyclic off-axis loading of an orthotropic composite are shown to follow the associated flow rule with a single-parameter quadratic potential function. The influence of fatigue damage on deformation is considerable due to the reduction in the elastic modulus of the composite and is apparently negligible with respect to its effect on the parameters of the creep kernel.Presented at the 10th International Conference on the Mechanics of Composite Materials (Riga, April 20–23, 1998).Translated from Mekhanika Kompozitnykh Materialov, Vol. 34, No. 4, pp. 447–460, July–August, 1998.     

A modified multistage fatigue model to study the fatigue life of forged HS6-5-3 tool steel under high cycle fatigue

DIN type forged HS6-5-3 tool steel (AISI M3:2) is most commonly used in tooling industry and also in some engine parts. Those components are usually exposed to cyclic mechanical stresses and 90% of them failed by fatigue damage. For predicting the life time of this tool steel under high cycle fatigue (HCF) a modified multistage fatigue model found by McDowell is proposed, which leads to reduce effects and cost for predicting life time of this material. (© 2013 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim)     

利用内聚力模型(CZM)模拟弹粘塑性多晶体的裂纹扩展

采用内聚力模型（CZM）,模拟多晶体中起裂于晶界的二维平面应变裂纹扩展．结果表明,弹粘塑性体中,初始裂纹尖端不会最先开裂．晶体本构的率敏感指数表征了塑性变形和内聚力区耗散两种机制的相互竞争．率敏感指数越大,塑性耗散能越大,内聚力区粘着能越小,使材料的塑性变形越容易,内聚力区诱发的破坏越不易;率敏感指数越小,材料响应越接近弹塑性性质,塑性耗散能减小,粘着能增大,外力功易转化为内聚力区的粘着能,使内聚力单元更易分离．增大内聚力区结合强度或临界张开位移使晶内和晶界的三轴应力度减小,即提高内聚力区韧性也使基体材料抗孔洞损伤能力提高．     

Microplane modeling of cyclic behavior of concrete: a gradient plasticity-damage formulation

A microplane model is developed to simulate the behavior of concrete under cyclic loading conditions. Pure damage mechanics or pure plasticity models yield satisfactory results for concrete under monotonic loading but cannot capture correctly the unloading and reloading response. Therefore, coupling damage and plasticity is necessary for accurate constitutive modeling of concrete. The microplane model offers a straightforward approach to simulate induced anisotropy by formulating the material laws on many randomly oriented planes. Distinguishing between compression and tension response using the proper plastic yield function and damage laws is considered. Furthermore, gradient enhancement is employed to handle the pathological mesh sensitivity related to strain softening. The new formulation is implemented within a 3D finite element code and a numerical example is simulated and compared to experiments in order to evaluate the capabilities of the model. (© 2016 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Fatigue strength and structure changes of polyethylene-oxide films under static and cyclic loading

Conclusions The behavior of the PEO films under long-term loadings show certain special features reflected mainly in the unusual form of the fatigue curve and the presence of three types of creep curves. The most significant factors affecting the fatigue characteristics of the PEO films are the molecular mass and the degree of crystallinity — when these factors increase the fatigue resistance also usually increases. To evaluate suitability of PEO films for service it is promising to use the cyclic bending test. This loading mode characteristic of practice makes it possible to carry out tests at low strain levels and cumulate considerable damage. Examination by the x ray diffraction method showed that in cyclically bent PEO films not only the amorphous but also crystalline structures are damaged.Translated from Mekhanika Kompozitnykh Materialov, Vol. 3, No. 3, pp. 404–412, May–June, 1994.     

PCB焊点热循环失效分析和改进设计

针对PCB（印制电路板）焊点在高低温热循环下的失效,建立了传统结构的三维模型和在芯片边角下加锡块的改进设计模型,通过实验测得FR-4的弹性模量和热膨胀系数,用ANSYS计算了PCB在高低温循环下的应力应变,并用修正的Coffin-Manson经验方程计算了焊点的热循环寿命。结果表明,通过在芯片边角下加锡块,PCB焊点的最大等效塑性应变显著降低,其热疲劳寿命得到明显提高.     

Fatigue damage modeling of fibrous soft tissues

Ultimate tendon failure is often caused by fatigue loading. Recent interventions revealed a three-phase progression of histological changes during cyclic loading of the tendon. It starts from localized kinked fiber deformations, continues with additional fiber delaminations and finally leads to fiber angulations and discontinuities [5, 6]. In the present contribution, we propose a physically motivated constitutive model able to describe fatigue evolution in tendon subject to cyclic loading. The damage of the collagen fibers is elucidated by a successive permanent opening of tropocollagen molecules [7], which represent the basic building blocks of collagen fibrils. The fibril strain increase is triggered by a time-force depending rupture of glycosaminoglycan sidechains of adjacent collagen fibrils. The so obtained model is in line with recent experimental findings available in literature. (© 2016 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Plastic limit analysis and optimum design of structures for uncertain conditions.

At the application of the plastic analysis and design methods the control of the plastic behaviour of the structures is an important requirement. Since the plastic limit analysis provides no information about the magnitude of the plastic deformations and residual displacements accumulated before the adaptation of the structure, therefore complementary strain energy of the residual forces could be considered an overall measure of the plastic performance of structures and the plastic deformations should be controlled by introducing a bound for magnitude of this energy. If the design uncertainties (manufacturing, strength, geometrical) are expressed by the calculation of the complementary strain energy of the residual forces a reliability based extended plastic limit design problem is formed. In this research, due to the uncertainties the bound for the complementary strain energy of the residual forces is given randomly and a general approach to evaluate the limit load capacity of structures for uncertain conditions is presented. The aim of this study is to evaluate limit load capacity of structures with limited residual strain energy on the probabilistically given conditions. (© 2016 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim)