不同方式预应变TiNi合金丝的马氏体逆相变温度

对恒应力约束下降温预应变和室温拉伸预应变TiNi形状记忆合金丝的马氏体逆相变行为进行研究.结果表明,随着预应变的增加,二者的马氏体逆相变温度都上升,应变回复率都下降;但是在相同预应变下,前者的马氏体逆相变温度低于后者,后者的应变回复率却高于前者.     

TiNi和TiNiCu记忆合金丝/镍基机敏复合材料相变潜热研究(英文)

通过DSC对TiNi和TiNiCu记忆合金丝/镍基机敏复合材料的相变潜热进行了研究.结果表明,预应变TiNi试样在无约束状态下的第一次马氏体逆相变过程中,相变潜热值随预应变水平的增加而迅速增大,而在镍基体约束下,相变潜热值随预应变水平的增加而迅速减小.但TiNiCu和TiNiCu丝/镍基复合材料的相变潜热变化趋势与TiNi试样的明显不同.对上述现象给出了合理的解释.     

NiTi形状记忆合金丝在Al基复合材料的约束态马氏逆相变特征

利用DSC,XRD,SEM等实验手段研究了NiTi记忆合金丝在铝合金丝在铝基体约束状上的马氏体逆相变特征,研究结果表明,预应变NiTi记忆合金丝在加热过程中发生两种马氏体逆相变,热致马氏体转变（M^T→P) 应力诱发马氏体逆转变（M^d→P）,其中热致马氏体相变温度与未预应变样品基本相同,且不受参应变影响,而应力诱发马氏体向母相转变温度随预应变增加而升高,随预应变增加,热致马体与应力诱发马氏体的转变时减少,文中引入马氏体变形度概念,并对马氏体在逆转变过程中的变形度变化进行了讨论。     

NiTi形状记忆合金丝在Al基复合材料中的约束态马氏体逆相变特征

利用DSC,XRD,SEM等实验手段研究了NiTi记忆合金丝在铝基体约束状态下的马氏体逆相变特征。研究结果表明,预应变NiTi记忆合金丝在加热过程中发生两种马氏体逆相变：热致马氏体逆转变(MT→P)与应力诱发马氏体逆转变(Md→P),其中热致马氏体逆相变温度与未预应变样品基本相同,且不受预应变影响;而应力诱发马氏体向母相转变温度随预应变增加而升高;随预应变增加,热致马氏体与应力诱发马氏体的逆转变量减少。文中引入马氏体变形度概念,并对马氏体在逆转变过程中的变形度变化进行了讨论。     

TiNi形状记忆合金在定应变约束下的马氏体相变

通过DSC及回复应变的测量,研究了定应变约束态加热-冷却过程对预应变TiNi形状记忆合金相变行为的影响。结果表明,在约束态相变中,逆相变温度区间拓宽;取向马氏体除向母相转变外,应变还要进一步增大;在正相变过程中,从母相生成的马氏体也具有变形结构。约束态不完全相变后,样品中存在两种马氏体;再变形马氏体和继承变形马氏体,在随后的无约束逆相变过程中,前者的相变温度高于后者,并且输出两段回复应变。     

TiNi合金在恒应力约束下的不完全相变

利用DSC对预应变TiNi形状记忆合金丝在恒应力约束下的马氏体不完全逆相变进行了研究,发现不完全相变热循环样品在第二次自由态加热过程中出现两步马氏体逆转变和两段应变回复现象.分析认为:经过恒应力约束下的不完全逆相变后,TiNi样品中存在不同的马氏体,在随后的加热过程中先后逆转变,产生两段回复应变.     

Ni含量对激冷贫镍TiNi形状记忆合金薄带相变行为的影

用激冷甩带法制备了Til-xNix(x=45％～49.8％)(原子分数)形状记忆合金(SMA)薄带,用示差扫描量热仪研究了Ni含量对铸态及450℃、500℃退火态TiNi SMA薄带相变行为的影响.结果表明,冷却/加热时,铸态和退火态Ti1-xNix(x=45％～49％)SMA薄带发生A→M/M→A一阶马氏体相变;当Ni含量为49.8％时,铸态和退火态TiNi SMA薄带冷却时发生A→ R→M两阶段相变,加热时发生M→A一阶段相变.随Ni含量增加,TiNi SMA薄带马氏体正、逆相变温度范围先增大后减小,Ni含量为48％时相变温度范围最宽.退火态比铸态TiNi SMA薄带相变温度范围窄.随Ni含量增加,TiNi SMA薄带马氏体正、逆相变温度升高,相变热滞增大.当Ni含量为49％时,SMA薄带的马氏体相变温度达最大值,当Ni含量为49.8％时马氏体相变温度迅速下降.     

Ni含量对激冷贫镍TiNi形状记忆合金薄带相变行为的影响

用激冷甩带法制备了Ti_(1-x)Ni_x(x=45%~49.8%)(原子分数)形状记忆合金(SMA)薄带,用示差扫描量热仪研究了Ni含量对铸态及450℃、500℃退火态TiNi SMA薄带相变行为的影响。结果表明,冷却/加热时,铸态和退火态Ti_(1-x)Ni_x(x=45%~49%)SMA薄带发生A→M/M→A一阶马氏体相变;当Ni含量为49.8%时,铸态和退火态TiNi SMA薄带冷却时发生A→R→M两阶段相变,加热时发生M→A一阶段相变。随Ni含量增加,TiNi SMA薄带马氏体正、逆相变温度范围先增大后减小,Ni含量为48%时相变温度范围最宽。退火态比铸态TiNi SMA薄带相变温度范围窄。随Ni含量增加,TiNi SMA薄带马氏体正、逆相变温度升高,相变热滞增大。当Ni含量为49%时,SMA薄带的马氏体相变温度达最大值,当Ni含量为49.8%时马氏体相变温度迅速下降。     

膨胀法分析Fe-1 7 Mn-1 0 Cr-5 Si-4 Ni形状记忆合金的恢复特性

利用Formaster FTM-4型膨胀仪对Fe-17Mn-5Si-10Cr-5Ni合金的形状恢复特性进行了分析,测得了恢复应变随加热温度变化的连续曲线。结果表明,合金在加热恢复前后,其热线性膨胀系数基本不变;合金发生ε→γ马氏体逆相变的起始温度As和预变形量无关,而终止温度Af随预变形量的增加而升高;试样在恢复过程中,前期和后期恢复较慢,中期恢复较快;合金的形状恢复率随预变形量的增大而降低;但最大可恢复应变出现在预变形量为5％左右。     

外加载荷对热弹性马氏体正-逆相变影响机制的相场模拟研究

本工作建立了一种新的马氏体逆相变的相场模型,以Cu-Al-Ni合金为例,研究了热弹性马氏体正相变和逆相变的演化规律,揭示了热弹性马氏体的形状记忆效应。同时模拟了拉伸释放弹性应变能这种机制对热弹性马氏体相变和热弹性马氏体逆相变的作用,研究了外加载荷对马氏体逆相变温度As的影响。模拟结果表明：应变能是形状记忆合金马氏体相变的阻力,是其逆相变的驱动力。在马氏体正相变过程中,拉伸载荷释放了应变能,降低了相变阻力,从而对马氏体相变起促进作用;在马氏体的逆相变过程中,由于拉伸载荷降低了马氏体所储存的应变能,因而降低了逆相变过程的驱动力,使合金逆相变As温度升高,进而提高了热弹性马氏体的低温稳定性。模拟结果与实验结果相一致。     

热循环对预应变NiTi记忆合金丝/铝基复合材料马氏体逆相变的影响

采用热压法将0.26mm的NiTi合金丝复合于铝中,利用SEM,DSC,热膨胀仪等实验手段研究了热循环对预应变为4%的NiTi合金丝/铝基复合材料马氏体逆相变的影响。结果表明,在第一次加热过程中,马氏体逆转变开始温度明显升高;第二次加热过程中逆转变开始温度比未预应变样品略有降低;随热循环次数增加,逆相变开始温度降低;当循环次数超过30次后,逆转变温度几乎保持不变。并对热循环过程中的马氏相变过程进行了分析讨论。     

Martensitic Transformation of TiNi Shape Memory Alloy Fiber Reinforced Ni Matrix Composites

In this paper, a TiNi shape memory alloy fiber Ni matrix composite was fabricated by an electroplating method using TiNi alloy as the cathode and Ni as the anode. The constrained martensitic transformation behaviors of the TiNi alloy were studied by differential scanning calorimeter (DSC), and the results showed that two endothermic peaks appear on the DSC heating curves and the reverse transformation temperatures increase with increasing prestrain levels. Moreover, comparing to the free transformation, the temperature window of the constrained reverse transformation is widely expanded due to the influence of recovery stress.     

Separation of the Martensite in TiNi Fiber Reinforced Aluminum Matrix Composite

The reverse martensitic transformation of TiNi shape memory alloy fibers embedded in a pure aluminum matrix was studied in this paper. Results showed that the phase composition of the TiNi alloy fibers prior to prestraining at the room temperature had a significant influence on the differential scanning calorimetry (DSC) results of the composites. By a comparison to the high temperature X-ray diffraction (XRD) results, it was confirmed that the martensite was divided into two groups: the self-accommodating martensite (SAM) and the preferentially oriented martensite (POM). The evolving process of the separation of martensite was discussed.     

Factors Affecting Transformation Temperatures in Fe-Mn-Si-Cr-Ni Shape Memory Alloy

1. IntroductionFe-Mn-St-Cr-Ni shape memory alloys exhibit notonly a good shape memory effect (SME), but also agood corrosion resistanced'2] ) compared with Fe-MuSt alloys. Fulthermore, it can be used in manufacturing pipe couplings because of its high phase transformation temperatures and great thermal hysteresis.But the recovery strain in these alloys is still low (lessthan 2%), which licits their application in pipe couplings. Therefore, to increase the recovery strain iskey to their pra…     

Effect of prestrain on tensile property of TiNif/Mg composite

A TiNi shape memory alloy fibre-reinforced AZ31 Mg alloy matrix composite was fabricated herein by spark plasma sintering. The microstructure of the composite and the effect of prestrain on its strength were analysed. The phase transformation of TiNi was observed in situ, and the effect of temperature was monitored. Metallurgical bonding formed at the interface between the TiNi fibre and AZ31 matrix. The prestrain strengthening effect on the yield stress of the composite at 298?K was more dramatic than at 373?K, and the effect decreased with increasing prestrain. The prestrain strengthening effect on tensile strength of the composite was effective at both 298 and 373?K. Because of the difference between recovery stress of TiNi and prestrain-induced compressive stress, higher temperature strengthened the material more significantly than did prestrain application.     

Two-stage recovery strain of prestrained TiNi shape memory alloy after phase transformations under constraint

A two-stage strain recovery was observed in a TiNi alloy fiber, which had been prestrained and experienced a constraint heating and cooling cycle with a fixed strain constraint. The results of differential scanning calorimeter (DSC) measurements showed that after the thermomechanical process, the self-accommodation martensite in the TiNi alloy was divided into two sorts of martensite, the redeformed martensite and the inheriting deformation martensite. The first stage of the recovery strain vs. temperature curve corresponds to the transformation from the inheriting deformation martensite to parent, and the second one corresponds to the transformation from the redeformed martensite to parent.