首页> 外文会议>Conference on Active Materials: Behavior and Mechanics Mar 3-6, 2003 San Diego, California, USA >Initial Investigation in Actuator Design Using High Temperature Shape Memory Alloy
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Initial Investigation in Actuator Design Using High Temperature Shape Memory Alloy

机译:使用高温形状记忆合金进行执行器设计的初步研究

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The need for shape memory alloys (SMA) with high transformation temperatures is urgent. SMA actuators may then be designed that will demonstrate two important attributes: (ⅰ) actuation in a high temperature environment and (ⅱ) high actuation frequency in a moderate temperature environment. Copper-Aluminum-Nickel (CuAlNi) single crystal alloy is a promising candidate due to favorable characteristics such as wide range of transformation temperatures, large actuation stress and strain, and lack of plastic deformation under cyclic loading. These characteristics point to the possibility that CuAINi single crystal high temperature SMA (HTSMA) actuators can be developed that will demonstrate the attributes mentioned above. An initial investigation of these possibilities is carried out computationally by analyzing a HTSMA-actuated airfoil. An existing rate-independent thermomechanical model is calibrated to describe the CuAINi material behavior. Time-dependent thermomechanically-coupled parametric studies are carried out to yield information about the airfoil stroke (trailing edge deflection), the actuation energy required and the actuation frequency possible for cyclic actuation, all as a function of transformation temperatures. For comparison purposes, a similar parametric study is also carried out for NiTi polycrystalline SMA. The analysis indicates that a CuAINi HTSMA actuated airfoil will demonstrate a cooling time two to six times lower than its NiTi SMA counterpart.
机译:迫切需要具有高相变温度的形状记忆合金(SMA)。然后可以设计出具有两个重要属性的SMA致动器:(ⅰ)在高温环境中致动,以及(ⅱ)在中等温度环境中致动频率高。铜铝镍(CuAlNi)单晶合金具有良好的特性,例如相变温度范围宽,致动应力和应变大,并且在循环载荷下缺乏塑性变形,因此是有前途的候选材料。这些特性表明,可以开发出CuAINi单晶高温SMA(HTSMA)执行器以证明上述属性的可能性。通过分析HTSMA驱动的机翼,对这些可能性进行了初步研究。校准了一个与速率无关的现有热力学模型,以描述CuAINi材料的行为。进行与时间有关的热机械耦合参数研究,以得出有关机翼冲程(后缘偏斜),所需的驱动能量和循环驱动可能的驱动频率等信息,这些信息均是转变温度的函数。为了进行比较,还对NiTi多晶SMA进行了类似的参数研究。分析表明,CuAINi HTSMA驱动的机翼的冷却时间将比NiTi SMA的冷却时间短2至6倍。

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