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。     

NiTi纤维表面处理及其树脂基复合材料的界面特性

NiTi纤维表面呈惰性,表面能低,NiTi纤维与树脂间界面粘结性差.为了提高界面性能,采用硅烷偶联剂、表面涂层和低温冷等离子体技术等方法对NiTi纤维表面进行处理,改善纤维表面的浸润性,达到纤维与树脂界面良好的粘结.对复合材料进行界面剪切强度的测定,并利用扫描电镜观察拔脱纤维表面形貌的变化.研究表明:NiTi纤维经不同方法处理后,纤维的浸润性和界面的粘结强度均有不同程度的改变,其中冷等离子体处理的纤维再经硅烷处理,其复合材料IFSS提高2.94倍,ILSS提高1.45倍,且纤维与树脂粘合较好.     

NiTi纤维增强粘弹性基体与弹性基体复合材料的力学特性

借助Voigt混合律,针对马氏体逆相变过程,建立了NiTi纤维增强Kelvin粘弹性基体与弹性基体两种复合材料的应力-应变关系.在同样的升温过程及应力作用下,对两种复合材料的变形(应变)、约束态NiTi纤维逆相变开始温度进行了分析对比;升温、加载经历一段时间后,限制两种复合材料的应变为固定值,分析其受力特征.分析有助于了解NiTi纤维增强粘弹性基体与弹性基体复合材料的力学性能.     

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。     

界面相性态对纤维增强复合材料内应力传递的影响

本文用有限元法研究了具有基体裂纹的纤维增强复合材料内的应力传递问题。假设纤维与基体的界面为非理想的，文中运用“弹簧层”模型首先分析了在不同的组分弹性模量比、纤维体积含量与边界约束条件下，界面相性态对复合材料的应力传宾影响，然后进一步考察了在几种典型的损伤模式下界面附近的应力分布情况。     

热处理对NiTi形状记忆合金的相变的影响

对含Ti 50.8%的NiTi形状记忆合金在300℃、400℃、500℃保温不同时间进行时效处理,然后通过差示扫描量热仪DSC对其相变温度点进行测定,发现经时效处理调节后,Af最大可下降20~30℃左右,而Ms变化不大。通过不同时效温度和保温时间的DSC曲线比较,得出热处理对其相变温度点的影响规律,即在300~500℃时效处理时,保温时间越短,Af降低越明显,在相同保温时间时,保温温度越低,Af降低越明显。     

NiTi形状记忆合金纤维拔出中的力学问题

对NiTi 形状记忆合金纤维拔出的力学模型进行了探讨。在恒温状态下, 考虑纤维和基体间的界面摩擦力, 分别用两种本构理论, 即Tanaka 的指数模型和C. Liang 的余弦模型, 讨论了形状记忆合金纤维在变轴力作用下的拉伸问题。推导了形状记忆合金纤维拔出量的表达式, 并给出数值计算结果。由指数模型和余弦模型得到的结果非常吻合, 证明了这种理论方法是正确的。      

NiTi形状记忆合金疲劳行为的研究现状

NiTi形状记忆合金具有比其它同类合金更优良的力学性能、形状记忆效应、超弹性、阻尼特性和生物相容性等特点,广泛应用于工程、民用和医学领域.综述了NiTi形状记忆合金疲劳行为的研究现状;对其疲劳行为及其机制的研究,有助于进一步提高NiTi形状记忆合金的性能并延长它的寿命.     

界面相性态对纤维增强复合材料内应力传递的影响

本文用有限元方法,计算分析了办面相性态对纤维增强复合材料内纤维与机体的界面间应力传递的影响。分析结果表明,界面刚度系数是纤维增强复合材料内纤维与机体的界面间应力传递的主要影响因素。     

Effects of plate thickness on reverse martensitic transformation of prestrained NiTi/NiTi alloy

In this paper, differential scanning calorimeter (DSC) was used to study the effects of predeformation and plate thickness on the reverse martensitic transformation of explosively welded NiTi/NiTi alloy. Results showed that there was a constraint between Ni_50.4Ti (NiTi-1) and Ni_49.8Ti (NiTi-2), which led to that the thickness of NiTi-1 or NiTi-2 strongly affected the reverse martensitic transformation behavior because residual stress variations in thickness wound enable bias force to be built inside the composite. The DSC measurements showed that after deformation, the reverse martensitic transformation temperature of the composite was increased with the increasing thickness of NiTi-2. Also, the XRD results revealed that the microstructure of NiTi/NiTi alloy changed from B2 phase to B19’ phase along the thickness direction.     

形状记忆纤维热粘弹性基体复合材料的力学行为

应用热粘弹性理论和Voigt混合律,在变温场中针对马氏体逆相变过程建立了NiTi形状记忆纤维热粘弹性基体复合材料的应力-应变关系,在逆相变过程和基体呈现热粘弹态阶段,由于基体松弛其模量减小,在跃阶拉应力的作用下,复合材料的压缩应变迅速增大,纤维回复应力先增大后减小;在跃阶拉应变的作用下,复合材料的应力增加先变缓然后加快直至稳定,较高的温度和材料参数对NiTi纤维热粘弹性基体复合材料的力学行为和纤维的作动性能有明显的影响.     

Phase transformation behavior of porous NiTi alloy fabricated by powder metallurgical method

Nickel titanium shape memory alloys (NiTi-SMAs) were successfully produced from elemental Ni/Ti powders by powder metallurgical method and then subjected to age treatment. Microstructure was examined by SEM and XRD and phase transformation temperatures were measured by dilatometric method. The phase transformation temperatures increased with both duration and temperature of the age treatment. The porous product exhibited desirable shape memory effect.     

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。     

Effect of phase on debond strength in shape memory alloy reinforced composites

Systematic single fiber pullout tests were performed on epoxy composites embedded with nickel titanium shape memory alloy (SMA) wires. The SMA wires were tested in the austenitic or martensitic states to study and decouple the elastic moduli from martensite transformation or reorientation stresses in the analysis of debond loads. The results reveal that the SMA wires that were in the austenite phase consistently produced higher debond loads as compared to that of those wires that started in the martensite phase, likely due to differences in the Poisson’s ratio. Additionally, there appears to be a relationship between the elastic modulus and debond load where reinforcements with a higher elastic modulus displayed lower debond loads. Lastly, for SMA reinforcements that underwent a martensitic phase transformation or reorientation, the debond load was equivalent to the martensite transformation or reorientation load. The results of this work illustrate the sensitivity of SMA reinforced composites on the mechanical behavior and phase transformation characteristics of the constituent materials.     

热循环对NiTi合金焊接接头相变的影响

为了研究热循环对NiTi合金激光焊接接头相变行为的影响,用激光点焊了φ0.5 mmTi-50.6%Ni合金细丝,利用金相显微镜观察了母材和接头的显微组织,通过示差热分析仪研究了热循环对点焊接头相变行为的影响.结果表明,NiTi合金激光点焊接头,熔化区为树枝晶,热影响区由粗大等轴晶和细小等轴晶组成.热循环可改变接头的相变行为,使马氏体相变由B2→B19'转变为B2→R→B19'.随着热循环次数的增加,正相变过程中Rs点升高,R相变温度范围变宽,Ms点降低;逆相变的相变温度都降低.     

考虑纤维随机分布的复合材料热残余应力分析及其对横向力学性能的影响

建立了考虑纤维随机分布并包含界面的复合材料微观力学数值模型,模拟玻璃纤维/环氧复合材料固化过程中的热残余应力。通过与纤维周期性分布模型的计算结果进行对比,发现纤维分布形式会对复合材料的热残余应力产生重要影响,纤维随机分布情况下的最大热残余应力明显大于纤维周期性分布的情况下。研究了含热残余应力的复合材料在横向拉伸与压缩载荷下的损伤和破坏过程,结果表明:热残余应力的存在显著影响了复合材料的损伤起始位置和扩展路径,削弱了复合材料的横向拉伸和压缩强度。在横向拉伸载荷下,考虑热残余应力后,复合材料的强度有所下降,断裂应变显著降低;在横向压缩载荷下,考虑热残余应力后,复合材料的强度略有下降,但失效应变基本保持不变。由于热残余应力的影响,复合材料的横向拉伸和压缩强度分别下降了10.5%和5.2%。      

Transverse failure of carbon fiber composites: Analytical sensitivity to the distribution of fiber/matrix interface properties

An analytic differentiation method is presented to calculate the sensitivity of the transverse failure response of carbon fiber composite laminates to the distribution parameters of the fiber/matrix interface properties. The method starts with the evaluation of the sensitivities of the transverse failure response with respect to the interface properties of each fiber, ie, the cohesive failure strength and the critical displacement jump. These individual sensitivities are then used to calculate the sensitivities with respect to the mean and standard deviation of the interface properties. The derived sensitivities are implemented in a nonlinear interface-enriched generalized finite element method solver specially developed for this application. The interface-enriched generalized finite element method solver combines a cohesive modeling of the fiber/matrix interface failure with finite element meshes that do not conform to the composite microstructure. The approach is first demonstrated on a model material involving a one-dimensional domain containing N cohesive interfaces described by randomly selected cohesive failure properties. The method is then applied to the more complex problem of a composite laminate involving a large number of fibers.