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Isotropic Behavior of an Anisotropic Material: Single Crystal Silicon

机译:各向异性材料的各向同性行为:单晶硅

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Zero defect single crystal silicon (Single-Crystal Si), with its diamond cubic crystal structure, is completely isotropic in most properties important for advanced aerospace systems. This paper will identify behavior of the three most dominant planes of the Single-Crystal Si cube (110), (100) and (111). For example, thermal and optical properties are completely isotropic for any given plane. The elastic and mechanical properties however are direction dependent. But we show through finite element analysis that in spite of this, near-isotropic behavior can be achieved with component designs that utilize the optimum elastic modulus in directions with the highest loads. Using glass frit bonding to assemble these planes is the only bonding agent that doesn't degrade the performance of Single-Crystal Si. The most significant anisotropic property of Single-Crystal Si is the Young's modulus of elasticity. Literature values vary substantially around a value of 145 GPa. The truth is that while the maximum modulus is 185 GPa, the most useful <110> crystallographic direction has a high 169 GPa, still higher than that of many materials such as aluminum and invar. And since Poisson's ratio in this direction is an extremely low 0.064, distortion in the plane normal to the load is insignificant. While the minimum modulus is 130 GPa, a calculated average value is close to the optimum at approximately 160 GPa. The minimum modulus is therefore almost irrelevant. The (111) plane, referred to as the natural cleave plane survives impact that would overload the (110) and/or (100) plane due to its superior density. While mechanical properties vary from plane to plane each plane is uniform and response is predictable. Understanding the Single-Crystal Si diamond cube provides a design and manufacture path for building lightweight Single-Crystal Si systems with near-isotropic response to loads. It is clear then that near-isotropic elastic behavior is achievable in Single-Crystal Si components and will provide sub-second thermal equilibrium and sub-micron creep.
机译:具有金刚石立方晶体结构的零缺陷单晶硅(Single-Crystal Si)在对于先进航空航天系统重要的大多数特性中是完全各向同性的。本文将确定单晶硅立方体(110),(100)和(111)的三个最主要平面的行为。例如,对于任何给定的平面,热和光学性质是完全各向同性的。但是,弹性和机械性能取决于方向。但是,我们通过有限元分析表明,尽管如此,使用在最大载荷方向上具有最佳弹性模量的组件设计仍可以实现近乎各向同性的行为。使用玻璃粉粘结来组装这些平面是唯一不会降低单晶硅性能的粘结剂。单晶硅最显着的各向异性是杨氏弹性模量。文献值在145 GPa值附近变化很大。事实是,虽然最大模量为185 GPa,但最有用的<110>晶体学方向的高169 GPa,仍高于许多材料(例如铝和殷钢)的方向。并且由于该方向上的泊松比极低,为0.064,因此垂直于载荷的平面中的变形微不足道。当最小模量为130 GPa时,计算出的平均值接近最佳值,约为160 GPa。因此,最小模量几乎无关紧要。 (111)平面(称为自然劈开平面)经受住了冲击,由于其优越的密度,该冲击会使(110)和/或(100)平面超载。虽然各个平面的机械性能各不相同,但每个平面都是一致的,并且响应是可预测的。了解Single-Crystal Si金刚石立方体提供了设计和制造路径,用于构建对载荷具有近似各向同性响应的轻型Single-Crystal Si系统。显然,在单晶硅组件中可以实现近乎各向同性的弹性行为,并将提供亚秒级的热平衡和亚微米蠕变。

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