Minimization of the weight of the blade of the aerial installation by an adaptive hybrid optimization method

Konstantin Lapitan, Serhii Misura, Daria Listrova, Tetiana Rudenko, Ievgeniia Misura, Anatolii Vasiliev
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Abstract

In various fields of engineering practice, such as turbine building, power engineering, elements of thin-walled structures are widely used, which operate under increased loads when interacting with air or water. These include blades of impellers of radial-axial and rotary-blade hydraulic turbines, blades of wind power plants. Designing highly efficient machines and structures with the required level of reliability requires determining their optimal characteristics. The article proposes an adaptive method for finding the minimum of an arbitrary smooth multivariable function. The method was used to solve the benchmark optimization problem of a function in the form of a valley. The essence of the proposed algorithm lies in the sequential approach to the bottom of the valley and the subsequent movement in the direction of decreasing the objective function. Comparison of the results of calculating the minimum point of the function is performed using both non-gradient and gradient methods, namely: Powell, Hook-Jeeves, the steepest descent method and the developed method. It was found that the effectiveness of the proposed method is greater than the usual search algorithms, but it is not without its drawbacks. The method is proposed that represents a number of hybrid methods, which form a hybrid coalition Proposed hybrid algorithm does not provide a satisfactory result in the "single" search. The search algorithm reaches a point where all the values of the function at the surrounding points are greater than the values at the obtained point, and the algorithm cannot overcome the barrier. To solve the problem, it is necessary to take the obtained point as a new starting point and repeat the algorithm for finding the minimum of the function, that is, use the multistart method. The proposed method was used to solve the problem of optimizing the blade of an air installation, which was reduced to the problem of unconditional optimization using the method of penalty functions, but the goal function had a significantly valley structure. The optimal values of section thicknesses were obtained, which made it possible to build a blade with improved characteristics.
通过自适应混合优化法使空中装置叶片的重量最小化
在工程实践的各个领域,如涡轮机制造、电力工程等,薄壁结构元件被广泛使用,它们在与空气或水相互作用时承受着更大的载荷。其中包括径向轴流式和旋转叶式水轮机叶轮的叶片、风力发电厂的叶片。要设计出具有所需可靠性水平的高效机器和结构,就必须确定其最佳特性。文章提出了一种寻找任意平滑多变量函数最小值的自适应方法。该方法用于解决山谷形式函数的基准优化问题。所提算法的精髓在于依次接近谷底,随后向目标函数递减的方向移动。计算函数最小点的结果比较采用了非梯度法和梯度法,即Powell、Hook-Jeeves、最陡下降法和开发的方法。结果发现,所提出的方法比通常的搜索算法更有效,但也不是没有缺点。拟议的混合算法在 "单一 "搜索中不能提供令人满意的结果。搜索算法到达一个点时,周围点的所有函数值都大于所获点的值,算法无法克服这一障碍。要解决这个问题,就必须把得到的点作为新的起点,重复寻找函数最小值的算法,即使用多起点法。所提出的方法被用于解决空气装置叶片的优化问题,该问题被简化为使用惩罚函数方法的无条件优化问题,但目标函数具有明显的山谷结构。结果获得了截面厚度的最佳值,从而可以制造出具有更好特性的叶片。
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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