一种新的分布鲁棒优化方法及其在转子-定子间隙中的应用

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Xiao-Le Guan , Zhen-Xing Zeng , Hong-Shuang Li , Yuan-Zhuo Ma
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引用次数: 0

摘要

考虑结构构件生产和制造过程中固有的不确定性影响,稳健设计优化对于保证工程结构正常稳定的运行性能至关重要。然而,目前的鲁棒设计优化方法仍然相对保守、耗时,并且往往需要在结构性能上做出重大牺牲来实现鲁棒性。针对这些问题,本文提出了一种基于两级Kriging代理模型的分布式鲁棒优化(DRO)方法。构建第一级Kriging模型来取代设计变量与结构响应之间的关系,从而可以基于欧几里得范数和KL散度构建模糊集。这将内部最大化问题转化为确定性优化问题。随后,构建第二级Kriging模型,近似设计变量与最大期望值之间的关系,使外极小化问题也退化为确定性优化问题,再通过子集仿真优化进行求解。通过数值算例初步验证了所提方法的性能,并将该方法与某小型涡轮发动机动静间隙变化的确定性优化结果进行了比较,验证了所提方法的工程实用性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A new distributionally robust optimization method and its application to rotor-stator clearance
Robust design optimization is crucial for ensuring the normal and stable operational performance of engineering structures by considering the effects of uncertainties inherent in the production and manufacturing processes of structural components. However, current robust design optimization methods are still relatively conservative, time-consuming, and often necessitate significant sacrifice in structural performance to achieve robustness. In response to these issues, the present study proposes a novel distributionally robust optimization (DRO) method based on a two-level Kriging surrogate model. The first-level Kriging model is constructed to replace the relationship between design variables and structural response, thereby enabling the construction of ambiguity sets based on the Euclidean norm and Kullback–Leibler (KL) divergence. This transforms the inner maximization problem into a deterministic optimization. Subsequently, the second-level Kriging model is constructed to approximate the relationship between design variables and the maximum expected value so that the outer minimization problem is also degenerated into a deterministic optimization, which is then solved by subset simulation optimization. The performance of the proposed method is preliminarily validated through a numerical examples, after which its engineering practicability is demonstrated by comparing the results of DRO with those of deterministic optimization for the variation in rotor-stator clearance in a small turbine engine.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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