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Hybrid micro-macro-mechanical constitutive model for shape-memory alloys

机译:形状记忆合金的混合微宏力学本构模型

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A substantial reduction in the size of control actuation systems employed in today's aerospace vehicles can enhance overall vehicle performance by reducing envelope volume requirements and inert weight. Functional materials such as shape memory alloys (SMA's) offer the opportunity to create compact, solid-state actuation systems by virtue of the material's ability to convert electrical energy to thermal energy to mechanical energy within its microstructure. A hybrid micro-macro-mechanical SMA model is developed for future closed-loop actuator development studies. The constitutive model is a combination of concepts originally presented by Likhatchev for microstructural modeling and Brinson for modeling of transformation kinetics. Global strain of the heterogeneous solid or polycrystal, where the grains are assumed to be randomly oriented, was calculated by averaging the elastic, thermal, stress-induced and autoaccomodation strains of each grain over the total material volume. The introduction of a frequency distribution function in the micromechanical model provided a convenient way to quantify texture. The model was successfully tested under constant temperature conditions and constant load-low frequency cycling conditions.
机译:当今航空航天飞机中使用的控制致动系统尺寸的大幅减少,可以通过减少封套体积要求和惰性重量来提高整体车辆性能。诸如形状记忆合金(SMA's)之类的功能材料凭借其在微观结构内将电能转化为热能转化为机械能的能力,提供了创建紧凑的固态致动系统的机会。为将来的闭环执行器开发研究,开发了一种混合型微-宏-机械SMA模型。本构模型是由Likhatchev最初提出的用于微观结构建模和Brinson提出的用于转换动力学建模的概念的组合。通过将每个晶粒在总材料体积上的弹性,热,应力诱发和自适应应变进行平均,可以计算出其中晶粒被假定为随机取向的异质固体或多晶的整体应变。在微机械模型中引入频率分布函数提供了量化纹理的便捷方法。该模型已在恒定温度条件和恒定负载-低频循环条件下成功测试。

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