A Probabilistic Machine Learning Framework for Explicit Inverse Design of Industrial Gas Turbine Blades

Sayan Ghosh, Valeria Andreoli, G. A. Padmanabha, Cheng Peng, Steven Atkinson, Piyush Pandita, T. Vandeputte, N. Zabaras, Liping Wang
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Abstract

One of the critical components in Industrial Gas Turbines (IGT) is the turbine blade. Design of turbine blades needs to consider multiple aspects like aerodynamic efficiency, durability, safety and manufacturing, which make the design process sequential and iterative. The sequential nature of these iterations forces a long design cycle time, ranging from a several months to years. Due to the reactionary nature of these iterations, little effort has been made to accumulate data in a manner that allows for deep exploration and understanding of the total design space. This is exemplified in the process of designing the individual components of the IGT resulting in a potential unrealized efficiency. To overcome the aforementioned challenges, we demonstrate a probabilistic inverse design machine learning framework, namely Pro-ML IDeAS, to carry out an explicit inverse design. Pro-ML IDeAS calculates the design explicitly without costly iteration and overcomes the challenges associated with ill-posed inverse problems. In this work the framework will be demonstrated on inverse aerodynamic design of 2D airfoil of turbine blades.
工业燃气轮机叶片显式反设计的概率机器学习框架
工业燃气轮机(IGT)的关键部件之一是涡轮叶片。涡轮叶片的设计需要考虑气动效率、耐用性、安全性和制造等多个方面,这使得设计过程具有连续性和迭代性。这些迭代的顺序性迫使设计周期很长,从几个月到几年不等。由于这些迭代的反动性质,很少有人努力以一种允许深入探索和理解整个设计空间的方式积累数据。这在设计IGT的各个组件的过程中得到了例证,导致潜在的未实现的效率。为了克服上述挑战,我们展示了一个概率逆设计机器学习框架,即Pro-ML IDeAS,以执行显式逆设计。Pro-ML IDeAS明确地计算设计,而无需昂贵的迭代,并克服了与不适定逆问题相关的挑战。本文将对涡轮叶片二维翼型的反气动设计进行框架论证。
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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