疲劳寿命计退火特性及电阻变化推算载荷谱的研究

对三种交变应变量循环后的疲劳寿命计在不同温度下进行退火实验,由它们在低于再结晶温度退火后电阻去除量的不同,得出疲劳寿命计在交变应变作用下电阻累积的主要机理。根据疲劳寿命计的标定特性曲线和在载荷谱下的响应特性,由三个不同方向粘贴的疲劳寿命计电阻变化推算载荷谱,该方法扩大了疲劳寿命计的使用范围。     

温度/机械载荷作用下高强度刨链裂纹扩展的随机化分析

为了描述温度/机械载荷作用下裂纹扩展速率,基于疲劳和蠕变裂纹扩展的线形叠加模型,提取圆环链的材料参数,引入对数正态随机过程,建立温度/机械交变载荷共同作用下高强度圆环链的裂纹扩展随机模型,采用泰勒级数法获得指定裂纹长度下寿命分布和指定寿命下裂纹长度分析的表达式,并进行刨链裂纹扩展的实验测试研究.结果表明,建立的圆环链随机化模型与试验结果一致.     

316L不锈钢的高温疲劳蠕变行为和寿命预测

进行316L不锈钢在单级和两级载荷作用下的高温疲劳蠕变试验,研究了载荷历程效应对材料行为的影响.在已有统一的疲劳蠕变损伤演化模型基础上,得到了316L高温单级载荷作用下非线性损伤演化曲线.同时,建立了一种耦合载荷历程效应的多级疲劳蠕变载荷作用下的材料破坏准则.基于该破坏准则,结合材料的非线性损伤模型对316L不锈钢高温两级载荷作用下的疲劳蠕变寿命进行了预测,预测结果与试验数据符合得比较好.     

托盘用竹木复合层合板在疲劳/蠕变交互作用下断裂损伤研究

研究了在疲劳/蠕变交互作用下竹木复合层合板的断裂损伤行为.结果表明,在交变载荷最大值为75%的应力水平下,其疲劳/蠕变断裂曲线为3段式曲线;在55%的应力水平下,15小时内其疲劳/蠕变曲线为两段式曲线.随着最大载荷保持时间的增加,层合板的断裂寿命降低.在疲劳/蠕变交互作用下层合板的破坏形式主要为纤维撕裂、界面剪切破坏和层间开裂3种形式的综合表现.影响疲劳/蠕变断裂寿命分散性的因素主要有层合板的铺设结构、木材缺陷和竹材结构等的影响.     

疲劳/蠕变复合作用下聚苯乙烯的交互损伤研究

探讨了在疲劳／蠕变复合作用下聚苯乙烯的损伤交互作用，结果表明，在疲劳／蠕变复合作用下聚苯乙烯存在疲劳和蠕变的交互损伤，其断裂寿命比纯疲劳或纯蠕变的断裂寿命低；断裂机制是疲劳循环载荷松动和活化了分子链或链段，从而促进蠕变运动和断裂，并且，疲劳／蠕变的交互损伤程度与温度密切相关。     

保持时间对定向合金DZ125热/机械疲劳断裂行为的影响

对DZ125定向凝固铸造镍基高温合金进行了应变比为-1.0的同相位三角波和同相位梯形波,550℃()1000℃热/机械疲劳实验研究.实验结果表明:在相同应变幅下,同相位三角波载荷情况下的热/机械疲劳寿命比同相位梯形波载荷情况下的热/机械疲劳寿命长.研究了在两种载荷情况下材料的热/机械疲劳循环应力响应行为.试样断口的微观分析表明:在热/机械疲劳过程中,同时存在疲劳、蠕变和氧化损伤;在同相位三角波载荷下,穿晶 沿晶断裂为疲劳断裂的主要特征;在同相位梯形波载荷下,裂纹主要为沿晶萌生与扩展.这是导致在同相位梯形波载荷下疲劳寿命缩短的主要原因.     

交变载荷对CFRP复合材料-铝合金粘接接头剩余强度的影响

为了给碳纤维增强聚合物（CFRP）复合材料粘接结构的安全设计及应用提供参考,针对CFRP复合材料-铝合金对接接头,研究了拉-拉交变载荷作用下的疲劳寿命特性及剩余强度变化规律。设计专用夹具,完成接头的制作及固化,并测试其拉伸、剪切准静态失效强度,在此基础上进行不同载荷水平下的疲劳寿命测试。选取特定载荷水平,测试不同循环次数后的接头剩余强度,并对失效形式进行观察分析。结果表明:CFRP复合材料-铝合金对接接头强度-寿命（S-N）曲线在单对数坐标上符合线性函数规律;随着交变载荷循环周期的增加,接头剩余强度呈先慢后快的下降趋势,而且在较大的载荷水平下,下降幅度更为明显;经历交变载荷循环前、后接头失效形式发生改变,由局部CFRP复合材料表层撕裂转变为局部界面破坏。结合试验测试所获得的初始失效准则,并引入疲劳退化因子,建立内聚力模型对交变载荷作用下的粘接接头强度衰减进行数值模拟,结果表明所建立模型能够有效预测交变载荷作用下的接头剩余强度。      

DD3单晶合金高温蠕变、疲劳及其交互作用机制

研究不同温度、不同应力下DD3单晶合金不同取向的疲劳、蠕变及疲劳-蠕变交互作用机制.结果表明:给定的实验条件下,DD3单晶的疲劳、蠕变及其交互作用均具有明显的各向异性,均以[111]取向的寿命最长,[001]取向次之,[011]取向最短,在相同温度和应力条件下以疲劳时的各向异性程度最为显著;DD3单晶具有较强的抗蠕变能力和相对较弱的抗疲劳能力,疲劳-蠕变交互作用中蠕变起主要作用.     

蠕变/疲劳共同作用下寿命估算方法

通过载荷谱转换，将带保载时间的蠕变／疲劳循环用不带保载时间的纯疲劳循环代替，提出蠕变／疲劳共同作用时的寿命估算方法。对１２Ｃｒ１ＭｏＶ钢母材和焊材的蠕变／疲劳交互作用试验数据的分析结果表明，本方法方便、实用。提出一个表征蠕变／疲劳连续加载时交互作用行为的参数，蠕变／疲劳寿命比。分析认为，材料的蠕变疲劳交互作用行为与该比值的大小腾。材料在蠕变／疲劳共同作用下呈这是呈负交经作用，并非材料固有的特性，还取决于载荷条件。     

试样尺寸对定向合金DZ125热机械疲劳寿命的影响

对DZ125定向凝固铸造镍基高温合金进行了三种相位和两种试样尺寸的热机械疲劳实验研究.实验结果表明:在热机械载荷下,试样表面和内部温度梯度以及蠕变和氧化损伤的存在,导致试样工作段直径影响热机械疲劳寿命.当应变水平较高(疲劳寿命较短)时工作段直径为φ8mm试样的疲劳寿命和工作段直径为φ6mm试样的疲劳寿命无明显差别.当应变水平较低(疲劳寿命较长)时工作段直径为φ8mm试样的疲劳寿命比工作段直径为φ6mm试样的疲劳寿命长.     

Cumulative damage model based on equivalent fatigue under multiaxial thermomechanical random loading

A new creep–fatigue damage cumulative model is proposed under multiaxial thermomechanical random loading, in which the damage at high temperature can be divided into the pure fatigue damage and the equivalent fatigue damage from creep. During the damage accumulation process, the elementary percentage of the equivalent fatigue damage increment is proportional to that of the creep damage increment, and the creep damage is converted to the equivalent fatigue damage. Moreover, combined with a multiaxial cyclic counting method, a life prediction method is developed based on the proposed creep–fatigue damage cumulative model. In the developed life prediction method, the effects of nonproportional hardening on the fatigue and creep damages are considered, and the influence of mean stress on damage is also taken into account. The thermomechanical fatigue experimental data for thin‐walled tubular specimen of superalloy GH4169 under multiaxial constant amplitude and variable amplitude loadings were used to verify the proposed model. The results showed that the proposed method can obtain satisfactory life prediction results.     

高温合金材料时间相关热机械疲劳寿命预测技术

本文在变温非线性运动强化规律所描述的高温合金材料热机械疲劳应力－应变循环特性的基础上,重点讨论了应变控制的时间相关热机械疲劳寿命预测技术。对于温度循环的影响,采用由应变能密度表示的损伤参数,并且引入了温度损伤系数。对于循环时间的影响,引入了蠕变─疲劳相互作用的损伤机制,采用韧性耗散损伤模型。在确定模型的一些参数时,采用等温力学试验和疲劳试验的数据,把等温疲劳研究成果推广到变温疲劳分析领域。     

Cyclic stress-strain response during isothermal and thermomechanical fatigue

Isothermal high-temperature low-cycle fatigue and in-phase and out-of-phase thermomechanical fatigue tests were carried out on 316L austenitic stainless steel specimens controlled by computer. A non-linear kinematic hardening model with internal variables was used to simulate the cyclic stress-strain behaviour of isothermal fatigue. This model was modified by considering thermal cyclic effects in order to describe the cyclic stress-strain behaviour of thermomechanical fatigue (TMF) using only isothermal fatigue data and the material performance data. A very good approximation of the hysteresis loops was obtained by comparing with experiments of both in-phase and out-of-phase cases. The thermomechanical fatigue behaviour described by isothermal fatigue data gives the possibility of developing the TMF lifetime prediction technique.     

Auswirkungen der Schädigungsanisotropie auf die Lebensdauer von Stählen bei Zeitstandbeanspruchung

The effect of anisotropic damage on the rupture-time of steel under creep conditions The aim of the investigation is the prediction of the influence of creep history, e. g. pre-damage and pre-loading, on the further creep behaviour after changing the loading direction. The changing of the loading direction has a significant influence on the rupture-time. A model has been developed which describes the dependence of rupture-time from the anisotropic effect of damage.     

Effect of cyclic loading on subsequent creep behaviour and its implications in creep–fatigue life assessment

Abstract

Evaluation of creep–fatigue failure is essential in design and fitness evaluation of high-temperature components in power generation plants. Cyclic deformation may alter the creep properties of the material and taking cyclic effects into account may improve the accuracy of creep–fatigue failure life prediction. To evaluate such a possibility, creep tests were conducted on 316FR and modified 9Cr–1Mo steel specimens subjected to prior cyclic loading; their creep deformation and rupture behaviours were compared with those of as-received materials. It was found that creep rupture life and elongation generally decreased following cyclic loading in both materials. In particular, the rupture elongation of 316FR in long-term creep conditions drastically decreases as a result of being cyclically deformed at a large strain range. Use of creep rupture properties after cyclic deformation, instead of those of as-received material, in strain-based and energy-based life estimation approaches brought about a clear improvement of creep–fatigue life prediction.     

加载路径对5A06铝合金力学性能和微观组织的影响

目的 通过力学性能测试和微观组织表征等手段研究预加载方向和双向加载对5A06铝合金组织性能的影响。方法 分别沿轧制方向(RD)和垂直于轧制方向(TD)施加预变形,然后沿RD进行拉伸试验,对比研究预加载方向对合金力学性能的影响。通过双向拉伸试验研究合金在双向加载时力学性能的变化情况;采用透射电镜观察预加载和双向加载条件下典型试样内的位错组态,分析加载路径对位错组态的影响。结果 预加载使5A06铝合金的屈服强度提高,伸长率下降。与RD预加载相比,TD预加载对屈服强度和伸长率的影响更小,TD预加载试样的抗拉强度更高。不同预加载方向下试样的位错组态不同:预加载与二次加载方向一致会使位错沿单一方向塞积;预加载与二次加载方向垂直时会出现平行位错列交错缠结现象。双向加载时,不同加载比例下合金的应力–应变关系不同,加载比例越接近等比例双向拉伸情况,加工硬化系数越大,在等比例双轴拉伸时达到最大。在应力状态从单拉状态变化到等双拉状态的过程中,不同阶段屈服点间隔不同,在等比例双轴拉伸时达到最大,在单向拉伸时最小。对于不同加载比例的试样,其位错密度随中心区应变量的增大而增大。结论 预加载方向会显著影响5A06铝合金的力学性能和位错组态。不同比例的双向加载会影响5A06铝合金的应力–应变关系。     

Remaining life assessment of high temperature components using threshold stress concept

The paper first presents global experience, including that of our laboratory, mainly with power plant components to show that it is possible to extend the life of some critical components 2–3 fold over the design life. Different approaches for remaining life assessment are also briefly discussed. It appears that the main creep damage in so far as Cr-Mo and Cr-Mo-V steels are concerned, is an accumulation of creep strain. Hence, this paper suggests a new approach for creep life prediction based on threshold stress concept and stress-strain rate relationship. The approach is based on the analysis of creep and hot tensile data generated on a popular 1 Cr-0·3 Mo-0·25 V steel in the service exposed and the virgin states and also on samples with a wide range of microstructures prepared from the virgin states. A summary of the main finding leading to development of a new approach has been given.     

The characteristics of fatigue under isothermal and thermo-mechanical load in Cr–Ni–Mo cast hot work die steel

ABSTRACT High temperature isothermal fatigue (IF) and in-phase thermo-mechanical fatigue (TMF) tests in load control were carried out in cast hot work die steel. At the same load amplitude, the fatigue lives obtained in the in-phase TMF tests are lower than those obtained in the isothermal tests. Observations of fracture surface and the response of stress–strain reveal that cyclic creep in the tensile direction occurs and the intergranular cracks dominate in TMF tests, whereas cyclic creep in the compressive direction occurs and the path of the crack growth is mainly transgranular in IF tests. A model of life prediction, based on the Chaboche law, was discussed. Damage coefficients that are functions of the maximum temperature and the variation of temperature are introduced in the model so as to evaluate TMF lives in load control. With this method, the lifetime prediction gives results corresponding well to experimental data.     

Ratcheting‐fatigue behaviour of bainite 2.25Cr1MoV steel with tensile and compressed hold loading at 455°C

The ratcheting behaviour of a bainite 2.25Cr1MoV steel was studied with various hold periods at 455°C. Particular attention was paid to the effect of stress hold on whole‐life ratcheting deformation, fatigue life, and failure mechanism. Results indicate that longer peak hold periods stimulate a faster accumulation of ratcheting strain by contribution of creep strain, while double hold at peak and valley stress has an even stronger influence. Creep strains produced in peak and valley hold periods are noticeable and result in higher cyclic strain amplitudes. Dimples and acquired defects are found in failed specimen by microstructure observation, and their number and size increase under creep‐fatigue loading. Enlarged cyclic strain amplitude and material deterioration caused by creep lead to fatigue life reduction under creep‐fatigue loading. A life prediction model suitable for asymmetric cycling is proposed based on the linear damage summation rule.