Application of the Koch Curve to Increase the Strength of Aircraft Parts

L. Zhikharev
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Abstract

Fractals are formed by iterative repetition of the construction algorithm at different scale levels. The use of such an algorithm, which increases the strength properties during the construction of the structure, will strengthen these properties with each iteration. The Koch curve principle is applied in the article. Replacing the compressible plate with four new ones connected at angles increases the stability of the structure. This article theoretically confirms the increase in the stability of the Koch plate both at the level of individual plates and at the level of fractal segments and the structure as a whole (general stability). Regularities of stability changes at different scale levels with an increase in the number of iterations are established. A comparison of variants of Koch plates with different similarity coefficients is also carried out. The theoretical results were confirmed using simulations in the CAE system Solid-Works - a finite element analysis of the stability of computer models of the Koch plates was carried out. The graphs constructed from the obtained data correspond to the theoretical predictions of the dependence of stability on the geometric parameters of the Koch plate. As an illustration of the applicability of this kind of fractal structures in the design of aircraft parts, a fractal modification of a typical part, the slat rail, has been developed. The proposed modification of the rail was also investigated using computer simulations. A comparison of the strength properties of a standard-shaped part and its analogue with a fractal structure included showed the advantage of the latter: with certain values of mass and loading scheme, the fractal modification showed twice as much stability. This reduces the weight of the standard slat rail by 5% without loss of strength properties.
科赫曲线在提高飞机零件强度中的应用
分形是通过对构造算法在不同尺度上的迭代重复而形成的。使用这样的算法,在结构构建过程中增加强度属性,将在每次迭代中加强这些属性。本文应用了科赫曲线原理。将可压缩板替换为四块以角度连接的新板可以增加结构的稳定性。本文从理论上证实了科赫板块在单个板块水平、分形片段水平和整体结构水平上的稳定性增加(一般稳定性)。建立了不同尺度下稳定性随迭代次数增加的变化规律。并对不同相似系数的科赫板进行了比较。理论结果在CAE系统Solid-Works中得到了验证,并对科赫板计算机模型的稳定性进行了有限元分析。从所获得的数据构造的图形与稳定性依赖于科赫板几何参数的理论预测相对应。为了说明这种分形结构在飞机零件设计中的适用性,对典型零件板条导轨进行了分形改造。利用计算机模拟对提出的钢轨改造方案进行了研究。将标准件的强度特性与包含分形结构的模拟件的强度特性进行比较,发现了后者的优势:在一定的质量值和加载方案下,分形修饰的稳定性是后者的两倍。这在不损失强度特性的情况下,将标准板条轨道的重量减少了5%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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