基于fdqn的飞机薄壁零件公差闭环优化模型

IF 9.9 1区 工程技术 Q1 COMPUTER SCIENCE, ARTIFICIAL INTELLIGENCE
He Zhang , Yuan Li , Dong Xue , Xin Tong , Baihui Gao , Jianfeng Yu
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引用次数: 0

摘要

随着飞机产品的跨代发展,装配精度和性能的飞跃也带来了制造成本的显著增加。为了在不牺牲装配精度和性能要求的前提下降低成本、提高效率,公差优化是一个重要的研究方向。然而,当面对飞机装配中复杂的偏差关系和非线性优化时,公差优化过程受到采样量大、迭代计算频率高、相对独立性和智能水平低等因素的制约,逐渐暴露出其局限性。为了解决这些挑战,本研究提出了一种基于高分辨率-精度生成对抗网络(hares - precigan)和改进的Fick深度q -网络(FDQN)的容差闭环优化模型(TCOM)。该模型结合了拉丁超立方体采样(LHS)和hres - precigan,实现了对刚性和柔性装配偏差的有效公差分析。在此基础上,综合多个优化目标,利用FDQN对公差分配方案进行深度优化,使成本效益最大化。此外,设计了基于物理启发的勘探策略,通过菲克扩散机制实现非线性调节,提高模型优化的收敛性。通过一个具体的工业案例,从优化性能和优化方案两个方面对所提出的模型进行了评价。评价结果表明,改进后的探索策略在收敛性上比原有的epsilon-greedy策略提高了12.36%,在处理飞机装配公差优化问题时优于任何单一的元启发式算法。在公差优化方面,该模型显著提高了与成本效益相关的几个关键指标。该研究为公差优化提供了一种新的思路,旨在降低成本,提高效率,促进航空航天等领域高性能装配的智能化转型。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A FDQN-based tolerance closed-loop optimization model for thin-wall components in aircraft assembly
With the cross- generational development of aircraft products, the leap in assembly accuracy and performance has also brought about a significant increase in manufacturing costs. Tolerance optimization is a key research direction to reduce cost and increase efficiency without sacrificing assembly accuracy and performance requirements. However, when confronting complex deviation relationships and nonlinear optimization in aircraft assembly, the tolerance optimization process is constrained by factors such as large sampling volumes, high-frequency iterative calculations, relative independence, and low intelligence levels, gradually revealing its limitations. To address these challenges, a tolerance closed-loop optimization model (TCOM) based on a High Resolution-Precision Generative Adversarial Network (HiRes-PreciGAN) and improved Fick Deep Q-networks (FDQN) is proposed in this study. The model incorporates Latin Hypercube Sampling (LHS) and HiRes-PreciGAN to achieve efficient tolerance analysis of rigid and flexible assembly deviations. On this basis, the model synthesizes several optimization objectives, and uses FDQN to deeply optimize the tolerance allocation scheme to maximize the cost-effectiveness. In addition, an exploration strategy based on physical inspiration is designed to achieve nonlinear regulation through Fick diffusion mechanism to improve the convergence of model optimization. Through a specific industrial case, the proposed model is evaluated from the aspects of optimization performance and optimization scheme. The evaluation results show that the improved exploration strategy has a 12.36 % improvement in convergence compared with the previous epsilon-greedy strategy, and is superior to any single meta-heuristic algorithm when dealing with the tolerance optimization problem of aircraft assembly. In terms of tolerance optimization, the model significantly improves several key indicators related to cost-effectiveness. This study provides a new idea to tolerance optimization that aims to reduce costs and enhance efficiency, and facilitate the intelligent transformation in high-performance assembly for the aerospace and other fields.
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来源期刊
Advanced Engineering Informatics
Advanced Engineering Informatics 工程技术-工程:综合
CiteScore
12.40
自引率
18.20%
发文量
292
审稿时长
45 days
期刊介绍: Advanced Engineering Informatics is an international Journal that solicits research papers with an emphasis on 'knowledge' and 'engineering applications'. The Journal seeks original papers that report progress in applying methods of engineering informatics. These papers should have engineering relevance and help provide a scientific base for more reliable, spontaneous, and creative engineering decision-making. Additionally, papers should demonstrate the science of supporting knowledge-intensive engineering tasks and validate the generality, power, and scalability of new methods through rigorous evaluation, preferably both qualitatively and quantitatively. Abstracting and indexing for Advanced Engineering Informatics include Science Citation Index Expanded, Scopus and INSPEC.
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