Evaluation of Strain Hardening Parameters

The plane-strain compression test for three kinds of materials was carried out in atemperature range between room temperature and 400 ~C. The a- e curves and strain-hardeningrate at different temperatures were simulated and a reasonable fit to the experimental data wasobtained. A modified model created by data inference and computer simulation was developed todescribe the strain hardening at a large deformation, and the predicted strain hardening are in agood agreement with that observed in a large range of stress. The influences of different param-eters on strain hardening behaviour under large deformation were analysed. The temperatureincrease within the test temperatures for stainless steel 18/8 Ti results in dropping of flowstress and strain-hardening rate. For favourable r-fibre texture to obtain high r, the cold roll-ing was applied at large reduction. In the experimental procedure, the X-ray diffraction test wascarried out to compare the strain hardening and microstructure under large deformation for abcc steel (low carbon steel SS-1142). The results indicate that the high strain-hardening ratepossibly occurs when the primary slip plane {110} is parallel to the rolling plane and the strain-hardening rate decreases when lots of {110} plane rotate out from the orientation {110}//RP.     

Influence of Carbon Content on Strain Hardening Behaviour of Sintered Plain Carbon Steel Preforms

 Complete experimental investigation on the instantaneous strain hardening behaviour of powder metallurgy (P/M) preforms of pure iron, Fe-0.35%C, Fe-0.75%C and Fe-1.1%C was carried out. The strain hardening behaviour of the above-mentioned P/M sintered steel preforms with aspect ratio of 0.4 under triaxial stress state condition was determined by cold upsetting under nil/no and graphite lubricant conditions. The instantaneous strain hardening value (ni), strength coefficient (Ki), and the stress as a function of strain and densification were obtained and analyzed. Furthermore, a relation was obtained from a semi-log plot of stress against relative density and analyzed to study the hardening behaviour owing to densification as stress was a function of induced strain as well as densification in the P/M materials.     

Mg-xSn合金性能分析及Zn对Mg-0.4Sn合金性能影响

本文结合合金SEM相图,从合金晶粒大小和应变硬化指数两项指标出发分析了不同成分的Mg-xSn合金性能变化规律,结果表明,随着Sn含量增加合金的屈服强度和抗拉强度呈现先增高后降低的趋势,应变硬化指数逐渐降低。Zn的加入,显著提高了Mg-0.4Sn合金的力学性能,抗拉强度从95MPa提高到了169MPa,同时也使应变硬化指数下降。     

热镀锌双相钢应变硬化特性研究

研究了热镀锌双相钢的应变硬化特性,以及微观组织形态、锌层结构、拉伸条件等因素对应变硬化特性的影响。结果表明,典型的热镀锌双相钢拉伸曲线具有明显的阶段性。随着双相钢中马氏体含量的增加,材料的应变硬化指数快速下降;应变硬化指数与屈服强度呈现明显的负线性相关关系;合金化后的应变硬化指数有所降低,不同的拉伸速率、拉伸方向对应变硬化指数影响不显著。     

速率控制模式对GH4169高温合金拉伸性能的影响

通过对应变硬化指数、拉伸试验数据和微观晶粒形貌等进行分析,讨论了引伸计控制期间真应变在0.8%~1.6%,速率控制模式对GH4169高温合金室温(23±5)℃及高温(650±3)℃拉伸性能的影响。结果表明:室温下,应变控制模式测得的强度指标高于横梁位移控制模式测得的,而应变控制模式测得的塑性指标低于横梁位移控制模式测得的;高温下,应变控制模式与横梁位移控制模式测得的强度指标和塑性指标差异均可以忽略不计。     

高延性地质聚合物复合材料性能及微结构研究进展

基于桥联法则理论、经微观力学设计而成的高延性水泥基复合材料(HDCC)以其拉伸荷载下具有的多缝开裂和应变硬化性能而优于普通混凝土,然则其发展仍受制于高制备成本及碳排放。近10年来,绿色经济性地质聚合物/碱激发材料与纤维复合增韧的高延性复合材料(HDGC)得到研究与发展。本文在概述地质聚合物/碱激发材料反应机理及HDCC材料设计理论的基础上,主要综述了HDGC基本性能与微结构的已有最新研究进展。研究表明,制备HDGC具有可行性且制备的HDGC表现出高延性复合材料所具备的力学响应特点,包括压缩、拉伸应变硬化、界面微观力学、弯曲、抗冲击性能等。然而,受材料组成复杂等因素影响,HDGC力学和微结构依赖于地质聚合物/碱激发材料基体化学性质的改变。HDGC同时具有更小的裂缝宽度而利于材料自修复、较大收缩值以及潜在的良好耐久性。此外,基于有限研究,对比了HDGC与HDCC的相似与差异,以期更好地了解地质聚合物/碱激发材料被用作HDCC替代品时应注意的条件。最后进一步对HDGC存在的问题和研究方向做出了总结与展望。     

强塑性变形生产超细晶铁素体／马氏体双相钢

详细描述了通过等通道转角挤压（ECAP）＋临界区退火处理生产超细晶铁素体／马氏体双相（UFGF／MDP）钢的过程。本研究的目的，除了在应变梯度塑性原理中引入对增强应变硬化性产生影响的从几何学角度考虑必然会产生的高密度位错的理念外，还在于生产具有广泛应变硬化性（其它UFG材料几乎不具备）和超高强度及良好均匀延伸的UFGF／MDP钢。通过选择最佳的ECAP工艺路线以及临界区退火处理条件，能够生产出孤立的岛状UFG马氏体均匀地埋入UFG铁素体基体中的UFGF／MDP钢。根据ECAP过程中显微组织的变化探讨了在本研究的加工条件下这种独特显微组织的形成过程。UFGF／MDP钢的室温拉伸性能均优于粗晶对应钢种。更重要的是。尽管为UFG组织。但与其它UFG材料不同，本研究的UFGF／MDP钢从塑性变形开始就显现出广泛的应变硬化性，而这与晶粒尺寸无关。与应变梯度塑性有关。     

Low Cycle Fatigue Behavior and Deformation Mecha-nism of TWIP Steel

Low cycle fatigue behavior of TWIP （twinning induced plasticity） steel was investigated in axial symmetric tension-compression cyclic loading pattern. Fracture surfaces and microstructures were examined by optical, scanning electron and transmission electron microscopes. It was found that the fatigue life at the strain amplitude of 0.4 % is up to 15 000 cycles, which is much longer than TRIP780 and HSLAS00 steels. The strain hardening and softening features are significant until the strain amplitude comes to 1.25 ~. Persistent slip bands and tiny mechanical twinning layers were observed after fatigue deformation. Deformation mechanism of TWIP steel at low cycle fatigue process is not only twinning, but a complex of both twinning and persistent slip bands.     

Tensile Properties of TWIP Steel at High Strain Rate

 Tensile tests of TWIP steels of two compositions are performed in the strain rate range of 10-5-103 s-1. Results indicate that steel 1# does not exhibit TWIP effect but deformation induced martensitic transformation appears only. There exists TWIP effect in steel 3#. Tensile properties at room temperature are sensitive to strain rate in the studied strain rate ranges. Analysis on the relationship between strain hardening exponent and strain rates shows that strain induced martensitic transformation and formation of twins during deformation have significant influence on their strain hardening behavior.