He Zhang , Yuan Li , Dong Xue , Xin Tong , Baihui Gao , Jianfeng Yu
{"title":"基于fdqn的飞机薄壁零件公差闭环优化模型","authors":"He Zhang , Yuan Li , Dong Xue , Xin Tong , Baihui Gao , Jianfeng Yu","doi":"10.1016/j.aei.2025.103453","DOIUrl":null,"url":null,"abstract":"<div><div>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 <span><math><mi>Q</mi></math></span>-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.</div></div>","PeriodicalId":50941,"journal":{"name":"Advanced Engineering Informatics","volume":"66 ","pages":"Article 103453"},"PeriodicalIF":9.9000,"publicationDate":"2025-05-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"A FDQN-based tolerance closed-loop optimization model for thin-wall components in aircraft assembly\",\"authors\":\"He Zhang , Yuan Li , Dong Xue , Xin Tong , Baihui Gao , Jianfeng Yu\",\"doi\":\"10.1016/j.aei.2025.103453\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>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 <span><math><mi>Q</mi></math></span>-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.</div></div>\",\"PeriodicalId\":50941,\"journal\":{\"name\":\"Advanced Engineering Informatics\",\"volume\":\"66 \",\"pages\":\"Article 103453\"},\"PeriodicalIF\":9.9000,\"publicationDate\":\"2025-05-15\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Advanced Engineering Informatics\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1474034625003465\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"COMPUTER SCIENCE, ARTIFICIAL INTELLIGENCE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advanced Engineering Informatics","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1474034625003465","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"COMPUTER SCIENCE, ARTIFICIAL INTELLIGENCE","Score":null,"Total":0}
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 -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.
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.