An improved adaptive Kriging method for the possibility-based design optimization and its application to aeroengine turbine disk

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-08-14 DOI:10.1016/j.ast.2024.109495
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Abstract

Possibility-based design optimization (PBDO) can provide theoretical basis for the structural optimal design of fuzzy uncertainty model in engineering, so as to obtain the optimal design variables. The genetic algorithm (GA) based on adaptive Kriging method for PBDO requires high precision in the whole design space, while the region far from the limit state surface (LSS) of the constraint function has little effect on PBDO, thus greatly affects the computational efficiency. In order to improve the efficiency of PBDO, an improved adaptive Kriging method combined with active possibility constraint (I-AK-AC) is proposed in this paper. In I-AK-AC, the enhanced expected improvement learning function is first put forward to promote the convergence efficiency of Kriging model by reducing the accuracy of the region far from the LSS of the constraint function. Whereafter, the active possibility constraint is identified, and only the boundaries of active possibility constraint need to be approximated precisely by Kriging model. By these ways, the convergence speed of Kriging model is further ameliorated without affecting the computational accuracy, and the efficiency of PBDO is significantly improved. Three test examples and an engineering application of aeroengine turbine disk illustrate the validity and accuracy of the proposed I-AK-AC.

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用于基于可能性的设计优化的改进型自适应克里金法及其在航空涡轮盘中的应用
基于可能性的优化设计(PBDO)可以为工程中模糊不确定性模型的结构优化设计提供理论依据,从而获得最优设计变量。基于自适应克里金法的遗传算法(GA)用于 PBDO 对整个设计空间的精度要求很高,而远离约束函数极限状态面(LSS)的区域对 PBDO 的影响很小,因此大大影响了计算效率。为了提高 PBDO 的效率,本文提出了一种结合主动可能性约束的改进型自适应克里金方法(I-AK-AC)。在 I-AK-AC 中,首先提出了增强的预期改进学习函数,通过降低远离约束函数 LSS 区域的精度来提高克里金模型的收敛效率。之后,确定主动可能性约束,Kriging 模型只需精确逼近主动可能性约束的边界。通过这些方法,在不影响计算精度的前提下,进一步提高了 Kriging 模型的收敛速度,显著提高了 PBDO 的效率。三个测试实例和一个航空涡轮盘的工程应用说明了所提出的 I-AK-AC 的有效性和准确性。
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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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