汽车玻璃高温蠕变特性的实验与理论研究

通过对汽车用挡风玻璃进行不同温度、不同应力水平下的单轴拉伸蠕变实验,揭示了其非线性蠕变变形特性.实验发现,不同温度和载荷下的蠕变曲线形状类似,高温(550℃～590℃)下该材料的减速蠕变变形不很明显,主要表现为稳态和加速蠕变变形,且其断裂数据符合Monkman-Grant关系,应力和温度对其影响不显著.基于实验结果,本文建立了非线性高温蠕变本构方程.理论预测与实验数据进行了比较,结果表明所提出的本构方程能较好地描述汽车玻璃高温蠕变变形的全过程.     

蠕变——塑性交互作用的一种本构模型

基于热力学相容的本构模型并合理地定义广义时间，得到了描述蠕变、塑性及其交互作用的统一型本构方程。进而通过对在蠕变—塑性交互作用过程中材料内部子结构及其变化的分析，将材料的强化分解为对应于非弹性应变范围的强化和由蠕变变形导致的附加强化。对高温环境二维应力路径下３０４不锈钢的蠕变—塑性交互作用过程进行了分析，取得了与Ｏｈａｓｈｉ等的实验相吻合的结果。     

考虑损伤的内变量黏弹--黏塑性本构方程

基于Rice不可逆内变量热力学框架,在约束构型空间中讨论材料的蠕变损伤问题.通过给定具体的余能密度函数和内变量演化方程推导出考虑损伤的内变量黏弹--黏塑性本构方程.通过模型相似材料单轴蠕变加卸载试验对一维情况下的本构方程进行参数辨识和模型验证,本构方程能很好地描述黏弹性变形和各蠕变阶段.不同的蠕变阶段具有不同的能量耗散特点.受应力扰动后,不考虑损伤的材料系统能自发趋于热力学平衡态或稳定态.在考虑损伤的整个蠕变过程中,材料系统先趋于平衡态再背离平衡态发展.能量耗散率可作为材料系统热力学状态偏离平衡态的测度;能量耗散率的时间导数可用于表征系统的演化趋势;两者的域内积分值可作为结构长期稳定性的评价指标.     

考虑损伤的内变量黏弹-黏塑性本构方程

基于Rice 不可逆内变量热力学框架,在约束构型空间中讨论材料的蠕变损伤问题. 通过给定具体的余能密度函数和内变量演化方程推导出考虑损伤的内变量黏弹-黏塑性本构方程. 通过模型相似材料单轴蠕变加卸载试验对一维情况下的本构方程进行参数辨识和模型验证,本构方程能很好地描述黏弹性变形和各蠕变阶段.不同的蠕变阶段具有不同的能量耗散特点. 受应力扰动后,不考虑损伤的材料系统能自发趋于热力学平衡态或稳定态. 在考虑损伤的整个蠕变过程中,材料系统先趋于平衡态再背离平衡态发展. 能量耗散率可作为材料系统热力学状态偏离平衡态的测度;能量耗散率的时间导数可用于表征系统的演化趋势;两者的域内积分值可作为结构长期稳定性的评价指标.      

粘弹性固体的精细积分有限元算法

粘弹性固体本构方程的数学表达式分为微分型和积分型两种，其数值求解主要是时域上离散计算。文中从微分型表达式出发导出其状态空间方程的数学表达式，通过严格推导论证了它与微、积分型表达式的等价性；引入状态空间方程，从而利用精细积分格式来求解粘弹性固体本构方程；给出了粘弹性固体本构方程的精细积分有限元算法，为求解粘弹性固体本构方程的数值解提供了一个新的途径，具有计算简便，求解精度高等优点。     

SnPb钎料合金的粘塑性Anand本构方程

采用统一型粘塑性本构 Anand方程描述了电子封装焊点 Sn Pb钎料合金的非弹性变形行为 ,基于 Sn Pb 合金的弹塑性蠕变本构方程和实验数据 ,确定了6 2 Sn36 Pb2 Ag、6 0 Sn40 Pb、96 .5 Sn3.5 Ag和 97.5 Pb2 .5 Sn四种钎料合金 Anand方程的材料参数 ,验证了粘塑性 Anand本构方程对 Sn Pb合金在恒应变速率和稳态塑性流动条件下应力应变行为的预测能力。结果表明 ,Anand方程能有效描述 Sn Pb钎料的粘塑性本构行为 ,并可应用于电子封装 Sn Pb焊点的可靠性模拟和失效分析     

基于统计损伤理论的冻土蠕变本构模型研究

假定冻土粘塑性微元损伤符合修进的莫尔-库仑准则,损伤变量服从Weibull随机概型分布;基于热力学原理和统计损伤理论,通过推导得到了相关联流动法则下的蠕变损伤耦合本构方程.为了便于研究冻土蠕变和损伤的耦合作用,将提出的本构模型,通过用户子程序嵌入到有限元程序中.最后,对冻土中桩基承载力模型试验进行了数值模拟,结果表明:基于统计损伤理论的冻土蠕变本构模型能较好的模拟冻土蠕变变形的全过程,并且与实测蠕变变形十分吻合,该模型对冻土结构物长期稳定性分析和工程预测具有重要参考意义.     

热粘塑性体的积分－微分型本构关系

应用　　　关于应力是五维偏应变空间变形历史的泛函的概念和Ｖａｌａｎｉｓ有关内＊时理论的描述，本文提出，对热粘塑性体，应力可设为应变、应变率和温度历史的泛函；并应用Ｍｉｌｌｅｒ和其它一些作者有关内变量演化方程的描述，由此建立了热粘塑性体的积分－微分到本构方程．这一积分－微分型本构关系大体和Ｍｉｌｌｅｒ微分型模型等价．对１０２０钢的单轴本构响应进行了数值模拟，和Ｔａｎａｋａ与Ｍｉｌｌｅｒ的分析及一些实验结果符合较好．     

Sn—Pb共晶钎料合金的Bodner—Partom本构方程

采用Ｂｏｄｎｅｒ－Ｐａｒｔｏｍ粘塑性本构理论研究了Ｓｎ－Ｐｂ共晶合金的本构方程。在应变速率１０－５—１０－２Ｓ－１、温度为－５５—１２５℃的外部变量范围内进行了单轴拉伸和稳态蠕变数值模拟，结果与实验吻合良好。同时讨论了该本构方程用于ＳＭＴ焊点热循环寿命预测的实际意义。     

金属材料蠕变的微观热力学机理及本构方程的研究

蠕变是金属材料的重要现象，其机理及本构方程的研究则是其重要的研究领域。虽然这方面工作已为数颇多，但迄今尚难以与实验有较好的吻合。本文在综合前人各种蠕变机理的基础上，提出金属材料蠕变的热力学机理，并进而推导出蠕变的本构方程及里面变量应力和温度所满足的约束条件。其数值结果与试验较为一致。     

螺旋压缩弹簧应力松弛特性试验分析及其应用

本文通过应力松弛试验、理论推导及数值模拟研究了高温下螺旋压缩弹簧的应力松弛规律,并利用加速模型对工况下弹簧应力松弛服役寿命做出预测。首先,根据螺旋压缩弹簧的结构特点搭建了弹簧应力松弛连续动态测试装置,该装置不仅避免了传统测试方法存在的缺陷,而且能够保证试验过程中位移载荷恒定,并实时监测载荷变化。本文以某飞机舱门单锁机构中的螺旋压缩弹簧为试验对象进行了不同温度条件下的应力松弛试验,得到其松弛动力学曲线,并基于Arrhenius模型建立了弹簧在工况下的应力松弛服役寿命预测模型;其次,基于应力松弛和蠕变在本质上的一致性,结合金属材料蠕变规律并根据试验弹簧的受力特点,推导出用于描述试验材料松弛行为的蠕变本构方程,由试验结果获得该本构方程的材料常数;最后,通过该本构方程及材料常数,在ANSYS软件中对试验弹簧的松弛过程进行模拟,结果表明,模拟结果与试验结果误差不大于4%。因此,通过本文方法所建立的蠕变方程对弹簧在不同载荷条件下的应力松弛规律进行仿真分析具有一定的可行性与准确性。     

A thermodynamics based damage mechanics constitutive model for low cycle fatigue analysis of microelectronics solder joints incorporating size effects

Below certain length scales and in the presence of a non-uniform plastic strain field the mechanical behavior of many metals and its alloys is substantially different from that in bulk specimens. In particular, an increase in resistance with decreasing size has been observed in Pb/Sn eutectic solder alloys which are extensively used in microelectronics packaging interconnects. Due to the high homologous temperature, the Pb/Sn solder exhibits creep–fatigue interaction and significant time, temperature, stress and rate dependent material characteristics. The simultaneous consideration of all the above mentioned factors makes constitutive modeling an extremely difficult task. In this paper, a viscoplastic constitutive model unified with a thermodynamics based damage evolution model is embedded into a couple stress framework in order to simulate low cycle fatigue response coupled to size effects. The model is implemented into commercial finite element code ABAQUS. The microbending experiment on thin nickel foils is used to validate the model. Analyses are performed on a thin layer solder joint in bending under cyclic loading conditions.     

Multiaxial creep and cyclic plasticity in nickel-base superalloy C263

Physically-based constitutive equations for uniaxial creep deformation in nickel alloy C263 [Acta Mater. 50 (2002) 2917] have been generalised for multiaxial stress states using conventional von Mises type assumptions. A range of biaxial creep tests have been carried out on nickel alloy C263 in order to investigate the stress state sensitivity of creep damage evolution. The sensitivity has been quantified in C263 and embodied within the creep constitutive equations for this material. The equations have been implemented into finite element code. The resulting computed creep behaviour for a range of stress state compares well with experimental results. Creep tests have been carried out on double notched bar specimens over a range of nominal stress. The effect of the notches is to introduce multiaxial stress states local to the notches which influences creep damage evolution. Finite element models of the double notch bar specimens have been developed and used to test the ability of the model to predict correctly, or otherwise, the creep rupture lifetimes of components in which multiaxial stress states exist. Reasonable comparisons with experimental results are achieved. The γ^′ solvus temperature of C263 is about 925 °C, so that thermo-mechanical fatigue (TMF) loading in which the temperature exceeds the solvus leads to the dissolution of the γ^′ precipitate, and a resulting solution treated material. The cyclic plasticity and creep behaviour of the solution treated material is quite different to that of the material with standard heat treatment. A time-independent cyclic plasticity model with kinematic and isotropic hardening has been developed for solution treated and standard heat treated nickel-base superalloy C263. It has been combined with the physically-based creep model to provide constitutive equations for TMF in C263 over the temperature range 20–950 °C, capable of predicting deformation and life in creep cavitation-dominated TMF failure.     

Theory of creep deformation with kinematic hardening for materials with different properties in tension and compression

A constitutive model for creep deformation that describes the loading-history-dependent behavior of initially isotropic materials with different properties in tension and compression under stress vector rotations limited by 50–60° is presented within a thermodynamic framework. In the proposed constitutive model a kinematic hardening rule is adopted. This model also introduces an effective equivalent stress in the creep potential that is based on the first and second invariants of the effective stress tensor, and on the joint invariant of the effective stress tensor and eigenvector associated with the maximum principal Cauchy stress. The formulation of the kinematic hardening rule is presented and discussed. All the material parameters in the model have been obtained from a series of proposed basic experiments with constant stresses. These model parameters are then used to predict the creep deformation of the aluminum alloy under multiaxial loading with constant stresses, and under non-proportional uniaxial and non-proportional multiaxial loadings for both isothermal and nonisothermal processes.     

The constitutive representation of high-temperature creep damage

The elastic-viscoplastic constitutive equations of Bodner-Partom were applied to modeling creep damage in a high temperature Ni-alloy, B1900 + Hf. Both tertiary creep in bulk materials and creep crack growth in flawed materials were considered. In the latter case, the energy rate line integral C^* was used for characterizing the crack driving force, and the rate of crack extension was computed using a local damage formulation that assumed fracture was controlled by cavitation occurring within the crack-tip process zone. The results of this investigation were used to assess the evolution equation for isotropic damage utilized in the Bodner-Partom constitutive equations.     

DYNAMIC MECHANICAL BEHAVIOR OF 6061 AL ALLOY AT ELEVATED TEMPERATURES AND DIFFERENT STRAIN RATES

The compressive stress-strain relationships of 6061Al alloy over wide temperatures and strain rates are investigated. The dynamic impact experiments are performed using an improved high temperature split Hopkinson pressure bar apparatus. The experimental results are compared with those obtained by the modified Johnson-Cook constitutive model. It is found that the dynamic mechanical behavior depends sensitively on temperature under relatively low strain rates or on strain rate at relatively high temperatures. The good agreement indicates that it is valid to adopt the parameter identification method and the constitutive model to describe and predict the mechanical response of materials.     

A viscoplastic constitutive model with effect of aging

It is recognized experimentally that differences in plastic flow stress due to the change in strain rate of SUS304 stainless steel are found to decrease after cyclic preloadings, but minimal change is observed in relaxation properties. Therefore, viscosity function based on tensile stress–strain properties differs from that obtained from relaxation behavior. For such case, the existing visco-plastic constitutive concept, such as the so-called overstress model where only viscosity is taken into consideration, has a poor capability in predicting the time-dependent mechanical properties systematically. A new viscoplastic constitutive concept is presented to analyze the phenomenon. In the constitutive concept, the dynamic strain aging even at room temperature, as well as viscosity, are introduced as the dominant factors of the time-dependent plastic deformation. An experimental technique is proposed and some experimental results are presented to estimate the effects of aging and viscosity separately on the time-dependency of a SCM435 low alloyed steel under tensile loading. The proposed constitutive model with aging is verified for the systematical predictions of both plastic flow properties and relaxation behavior of the SCM435 low alloyed steel.     

电刷镀镍/镍包纳米Al_2O_3颗粒复合镀层微动磨损性能研究

应用电刷镀技术制备了含有镍包纳米 Al2 O3颗粒的镍基复合镀层 .与快速镍镀层对比考察了该复合镀层高温硬度的变化 ,同时还从微动磨损角度考察了该复合镀层耐磨性和摩擦系数的变化 .结果表明 :与快镍镀层相比 ,镍 /镍包纳米 Al2 O3复合镀层具有更高的高温硬度和更好的抗微动磨损性能 ;复合镀层在 40 0℃左右表现出较明显的强化趋势 ,具有较好的综合性能 ;纳米 Al2 O3颗粒使复合镀层的结构致密和细化 ,在磨损过程中起到了一定的减轻粘着和降低摩摩的作用 ;复合镀层的微动磨损机理主要为粘着磨损 .     

A constitutive theory for creep behavior of initially isotropic materials sustaining unilateral damage

The goal of the present work is to modify structure of the creep constitutive equations existing in the literature, and simultaneously to incorporate both damage induced anisotropy and unilateral damage into the constitutive model. The proposed nonlinear-tensor constitutive equation for creep together with the damage evolution equation take into account the secondary and tertiary creep of the initially isotropic materials. The material parameters of the model are determined using basic experiments. It is shown that the creep model is capable of describing available experimental data for the lateral creep responses under uniaxial compression.     

Predictions of nonlinear viscoelastic behavior using a hybrid approach

An approach for nonlinear viscoelastic characterization is presented which uses the combined measurements from creep and dynamic mechanical tests. Although the methodology should extend to several materials and geometries, this research concentrates on thin film polymers used in the manufacture of high altitude scientific balloons. Typically, the constitutive behavior of these materials is characterized through the use of linear viscoelastic techniques. Although this linear approach provides an accurate model for small strains or loads, these materials have been shown to be highly stress dependent and, consequently, it is necessary to identify this nonlinear behavior. Traditional creep measurements require extensive laboratory test times, yet the results obtained from dynamic mechanical analysis provide the capability to predict long term material performance without a lengthy experimentation program. However, dynamic mechanical methods are currently limited to linear response; thus, an approach is presented in which the stress-dependent behavior is derived from short-term creep measurements in a manner analogous to time-temperature superposition. Predictions of material response using linear and nonlinear approaches are compared with experimental results obtained from traditional long-term creep tests. Although linear pre-dictions deteriorate for large stresses, excellent agreement is shown for the nonlinear model.