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REDUCTION OF THE DESIGN SPACE TO OPTIMIZE BLADE FIR-TREE ATTACHMENTS

机译:减少设计空间以优化刀片杉木树附件

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The blade attachment, both dovetail or fir-tree, transfers the centrifugal load from the blade to the disc, generating high mean and peak stresses in notches as well as on contact surfaces. Hence, the strength of the attachment is one of the main concern of the designers for improving the performance of the engine and several optimization procedure have been put forward to minimize the state of stress in the attachment for a given centrifugal load. The optimization process is generally driven by a parametric model. The selection of the proper parameters and their variation ranges represent one of the main issues for the process to converge in a reasonable amount of time. Simulation methods and optimization algorithms have been improved a lot in the past years. Nevertheless, the computational effort of the finite element analysis involved in the optimization procedure of complex geometries remains a critical task. Moreover, an accurate evaluation of the local contact stresses is highly dependent on the mesh refinement, increasing the computing time of the whole optimization process. Moreover, a multi-objective optimization, in addition to robustness design approach, is the designer tool to improve the attachment performance. The searching domain reduction of the optimization process improves the computational performance reducing the convergence time of the solution. To achieve this goal, a preliminary selection of the design space has been performed by means of an analytical approach. This paper describes a new design criterion based on one dimensional approach. The criterion has been implemented in an in-house tool that takes faster decisions, if compared with a two or a three dimensional model, about the number of possible feasible solutions. During the geometrical optimization phase of the blade fir-tree attachment, in which a parametric model is used, the authors try to handle the geometrical non-feasibility with a combination of Latin Hypercube Sampling (LHS) and an adaptive penalty method. The optimization is done via the genetic algorithm and the computational time of the reduced domain is compared with the original one.
机译:燕尾形或枞树形的叶片附件将离心载荷从叶片转移到圆盘上,从而在槽口以及接触面上产生较高的平均应力和峰值应力。因此,附件的强度是设计者改善发动机性能的主要考虑之一,并且已经提出了几种优化程序以在给定的离心载荷下使附件中的应力状态最小化。优化过程通常由参数模型驱动。适当参数的选择及其变化范围代表了该过程在合理的时间内收敛的主要问题之一。近年来,仿真方法和优化算法已得到很大改进。然而,复杂几何形状优化过程中涉及的有限元分析的计算工作仍然是一项关键任务。此外,对局部接触应力的准确评估高度依赖于网格的细化,从而增加了整个优化过程的计算时间。此外,除健壮性设计方法外,多目标优化是提高附件性能的设计器工具。优化过程的搜索域减少可提高计算性能,从而减少解决方案的收敛时间。为了实现这一目标,已经通过分析方法对设计空间进行了初步选择。本文描述了一种基于一维方法的新设计准则。该标准已在内部工具中实施,如果与二维或三维模型相比,该工具可以更快地决定可能的可行解决方案的数量。在叶片枞树附件的几何优化阶段(其中使用了参数模型),作者尝试通过结合拉丁超立方体采样(LHS)和自适应惩罚方法来处理几何上的不可行性。通过遗传算法进行优化,并将缩小域的计算时间与原始域进行比较。

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