A “Point Cloud” Approach in Superelastic Stent Design

X. Gong, C. Bonsignore, A. Pelton
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Abstract

Figure 1 shows schematically the stress-strain relation for Nitinol under uniaxial tensile test at constant temperature. Originally, material is in the Austenite phase. Upon loading, below a small strain, ε1, stress is linearly proportional to the strain. The slope defines the Young’s modulus of Nitinol in Austenite phase. When strain reaches beyond ε1, a small increase in stress induces a large amount of strain owing to the phase transition from Austenite to Martensite. After completion of the phase transition, for strain larger than ε2, the stress and strain relation is linear again with a different slope, which defines the modulus of Martensite phase. During unloading, Martensite remains until strain ε3, which is less than ε2. Below ε3, the Martensite reverts to Austenite and a large reverse strain is produced until ε4, which is smaller than ε1. After unloading below ε4, the material returns to linear elastic behavior. This unique material behavior of Nitinol, known as superelasticity, along with its excellent biocompatibility and corrosion resistance, makes Nitinol a perfect material candidate for self-expanding stent applications. Self-expanding stents made of Nitinol offer unique features such as biased stiffness to better fit the anatomy and excellent corrosion resistance. When implanted in vivo, stents are subjected to the pulsatile loading from systolic and diastolic heartbeats and therefore it is necessary to design for a long (10 years) fatigue life. Nitinol’s fatigue behavior is known to depend upon the mean and the alternating strains from cyclic loading. Therefore, one approach to ensure that the stent has a long fatigue life is to design in such a manner that both the mean and the alternating strains of the proposed stent are lower than the Nitinol’s fatigue endurance limits. For linear materials, this normally is not an issue as the location of the maximum mean strain is also the location of maximum alternating strain, therefore the history of the maximum strain point can be used to predict the device fatigue life or used as the design criterion. However, Nitinol is a highly nonlinear and path dependent material that makes it possible that the location of the maximum mean strain is not necessarily the location of maximum alternating strain. A rigorous design criterion is developed at Nitinol Devices and Components (NDC) to trace the strain history of every material point. We accomplish this by means of a nonlinear finite element analysis (FEA) using ABAQUS. The FEA analysis uses a special user-defined material subroutine by HKS/WEST customized for Nitinol. The loading condition on the stents can come from two sources: 1. An analytical approach to determine the stent diameters by balancing the stent within a 6% compliant tube to simulate physiological loading, or 2. A direct measurement of stent diameter change inside the tube from the in-vitro testing. This article demonstrates the criterion using the second approach, i.e., the measured stent diameters are used as the FEA input. The mean and alternating strains at every element integration point or when extrapolated at every node produces a single point in the mean and alternating strain plane. The discretized stent produces “point clouds”. When this “point cloud” plot is superimposed on the fatigue endurance limit, the designer will have an idea of the relative safety of the design. The results are compared with the linear approach using traditional beam theory. It is verified that when the deformation is small, the beam theory agrees well with the nonlinear FEA analysis.
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超弹性支架设计中的“点云”方法
图1为镍钛诺在恒温单轴拉伸试验下的应力应变关系示意图。最初,材料处于奥氏体相。加载后,在小应变ε1以下,应力与应变成线性正比。斜率决定了镍钛诺在奥氏体相的杨氏模量。当应变大于ε1时,由于相变由奥氏体向马氏体转变,应力的小幅度增加引起大量应变。相变完成后,当应变大于ε2时,应力应变关系再次呈线性关系,但斜率不同,这决定了马氏体相的模量。卸载过程中马氏体一直保持到应变ε3,且小于应变ε2。在ε3以下,马氏体恢复为奥氏体,直至ε4,产生较大的反向应变,小于ε1。在ε4以下卸载后,材料恢复到线弹性状态。镍钛诺的这种独特的材料特性,被称为超弹性,以及其优异的生物相容性和耐腐蚀性,使镍钛诺成为自膨胀支架应用的完美候选材料。由镍钛诺制成的自膨胀支架具有独特的功能,如偏向刚度,以更好地适应解剖结构和优异的耐腐蚀性。当植入体内时,支架受到收缩期和舒张期心跳的脉动负荷,因此有必要设计长(10年)的疲劳寿命。已知镍钛诺的疲劳行为取决于循环载荷的平均应变和交变应变。因此,确保支架具有较长疲劳寿命的一种方法是设计支架的平均应变和交变应变均低于镍钛诺的疲劳耐力极限。对于线性材料,这通常不是问题,因为最大平均应变的位置也是最大交变应变的位置,因此最大应变点的历史可以用来预测设备的疲劳寿命或用作设计准则。然而,镍钛诺是一种高度非线性和路径依赖的材料,这使得最大平均应变的位置不一定是最大交变应变的位置。Nitinol Devices and Components (NDC)制定了严格的设计标准,以跟踪每个材料点的应变历史。我们通过使用ABAQUS进行非线性有限元分析(FEA)来实现这一目标。有限元分析使用HKS/WEST为镍钛诺定制的特殊自定义材料子程序。支架上的载荷条件可以有两个来源:1.支架上的载荷条件;一种分析方法来确定支架直径通过平衡支架在一个6%的柔性管模拟生理负荷,或2。通过体外试验直接测量导管内支架直径的变化。本文演示了采用第二种方法的判据,即使用测量的支架直径作为有限元分析的输入。在每个单元积分点的平均应变和交变应变,或者在每个节点外推时,在平均应变和交变应变平面上产生一个单点。离散支架产生“点云”。当这个“点云”图叠加在疲劳耐久性极限上时,设计师就会对设计的相对安全性有一个概念。结果与采用传统梁理论的线性方法进行了比较。结果表明,当变形较小时,梁理论与非线性有限元分析吻合较好。
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