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研究生: 林山瑞
Lingala Santhosh Reddy
論文名稱: 使用田口和多目標遺傳算法優化離心壓縮機設計
Optimization of a Centrifugal Compressor Design Using Taguchi and Multi-Objective Genetic Algorithm
指導教授: 賴維祥
Lai, Wei Hsiang
學位類別: 碩士
Master
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2022
畢業學年度: 110
語文別: 英文
論文頁數: 73
中文關鍵詞: 離心壓縮機田口法CFD次音速模型超音速模型
外文關鍵詞: Centrifugal compressor, Taguchi, CFD, Subsonic model, Supersonic model
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  • 摘要 I Abstract II Acknowledgment III Table of Contents IV List of Tables VII List of Figures VIII Nomenclature XI Chapter 1 Introduction 1 1.1 Background 1 1.2 Objective and Motivation 2 1.3 Literature review 3 Chapter 2 Description of Micro Turbine Engine 6 2.1 Micro Gas Turbine Engine 6 2.2 Turbocharger 8 2.2.1 Turbocharger construction 8 2.2.2 Center- housing 9 2.2.3 Bearings 10 2.2.4 Seals 10 2.2.5 The Compressor 10 2.2.6 The Compressor wheel 12 2.2.7 Types of compressor wheels 13 2.2.8 The compressor cover 17 2.3 The Turbine 22 Chapter 3 Research Methodology 23 3.1 Research Methodology Flowchart 23 3.2 Design and Analysis of Impeller 24 3.2.1 The Initial design for the subsonic model 25 3.3 Compressor map 28 3.4 Tip Clearance Analysis 29 3.5 Taguchi Analysis 31 3.5.1 Orthogonal array 32 3.5.2 Orthogonal array selection rules 33 3.6 RSO and DOE method to improve efficiency 34 3.6.1 GA methodology 35 3.6.2 ANSYS software DOE and RSO 36 3.6.2.1 Overview 36 Chapter 4 Results and Discussion 40 4.1 Results of subsonic model 40 4.1.1 Taguchi results 40 4.1.2 CFX results for subsonic model 44 4.1.2.1 Boundary condition settings 44 4.1.3 2nd stage of optimization using the DOE and RSO method 50 4.1.4 Optimized solid CAD model of a centrifugal compressor impeller 52 4.2 Results of a supersonic model 52 4.2.1 Taguchi results 52 4.2.2 CFX results for subsonic model 56 4.2.3 DOE and RSO results 61 4.2.5 Optimized solid CAD model 62 4.3 Comparing the results 63 Chapter 5 Conclusions and Future Work 65 5.1 Conclusions 65 5.2 Future Work 65 References 66 Appendix 69

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