簡易檢索 / 詳目顯示

研究生: 陳建志
Chen, Jian-Zhi
論文名稱: 微型渦輪發電系統之性能分析與模擬
Performance Analysis and Simulation of Micro Gas Turbine Generator System
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: 2019
畢業學年度: 107
語文別: 中文
論文頁數: 77
中文關鍵詞: 微型渦輪發電系統熱回收系統系統模擬參數研究法數值最佳化方法
外文關鍵詞: Micro-turbine power generation system, heat recovery system, System simulation, parameter study method, optimization method
相關次數: 點閱:82下載:0
分享至:
查詢本校圖書館目錄 查詢臺灣博碩士論文知識加值系統 勘誤回報
  • 本研究主要目的為建立一60 kW級之微型渦輪發電系統,並且搭配復熱器及廢熱鍋爐之熱回收系統,分析方法為利用商用套裝軟體GasTurb11作為系統模擬之工具,選擇參考離心式渦輪增壓器TD-08H做為系統模擬之重要設計參數,渦輪增壓器之質量流率為0.55 kg/s、壓縮比(γ)為3.2,在空氣條件為海平面288.15 K、空氣濕度60%、大氣壓力101.325 kPa進行設計點分析。
    本研究先利用敏感性分析法找出對系統性能影響程度較大之設計參數,進一步以參數研究法探討重要參數對系統之性能及各站位氣體性質之影響,得出渦輪發電系統之新設計點,再以數值優化方法驗證該設計點為最佳熱力循環操作點。最後針對熱回收配置進行分析,以各復熱器有效性條件下之渦輪發電系統性能作為配置廢熱鍋爐之參考依據,得知欲達到系統設計目標,復熱器有效性90%時,鍋爐最少熱回收量為68 kW,實驗結果得到系統輸出功為64.1 kW,熱電效率34.64%,成功模擬得到高效率渦輪發電系統之設計參數。

    The main purpose of this paper is to establish a 60 kW micro-gas turbine power generation system with heat recovery system by a recuperator and a heat recovery boiler. The study method is using the commercial package software GasTurb11 for the gas turbine system simulation tool. The centrifugal turbocharger TD-08H is selected for the system simulation as important design parameters. The turbocharger has mass flow rate of 0.55 kg/s, compression ratio (γ) of 3.2. The design point analysis is also simulated at the air condition 288.15 K at sea level, 60% air humidity, and atmospheric pressure 101.325 kPa.
    In this study, using the sensitivity analysis method can find out which design parameters is much more effective on the system performance. The parameter study method is used to investigate the influence on the system performance and the gas properties on each station. Then, new design point of the turbine power generation system is obtained. Simultaneously, the study using optimization method verify the new design point as the optimal thermodynamic cycle operation point. Finally, the heat recovery configuration is analyzed by the condition of system performance with difference recuperator effectiveness, and we can know the rated power of heat recovery boiler. If the system would like to meet the requirement of design target, the 90% effectiveness recuperator system needs to cooperate with a 68 kW rated power of heat recovery boiler.
    The experimental results show that the system output power is 64.1 kW and the thermal efficiency is 34.64%. The design parameters of the high efficiency turbine power generation system are successfully simulated.

    中文摘要 I Performance Analysis and Simulation of Micro Gas Turbine Generator System II 誌謝 V 目錄 VI 表目錄 IX 圖目錄 XI 符號 XIII 第1章 緒論 1 1-1 前言 1 1-2 研究動機 3 1-3 文獻回顧 5 1-4 研究目的與方法 9 第2章 系統設計與理論分析 12 2-1 燃氣渦輪理想循環 12 2-2 系統設計 19 2-2-1 系統設計概念 19 2-2-2 熱回收系統 22 2-3 系統規劃 25 第3章 氣渦輪模組建立 28 3-1 系統設計目標及需求 28 3-2 氣體產生器 30 3-3 動力渦輪 33 3-4 復熱器系統(Recuperator System) 35 第4章 設計點分析 38 4-1 初步基礎參數設定 38 4-1-1 初始系統(Initial System) 38 4-1-2 復熱器系統 42 4-2 敏感性分析(Sensitivity Analysis) 47 4-3 參數研究(Parametric Study) 50 4-3-1 等熵效率參數研究 50 4-3-1 燃燒室出口溫度 56 4-3-2 復熱器參數研究 62 4-3-3 數值最佳化驗證 65 4-4 熱回收最適化配置方案 67 第5章 結論 74 5-1 結論 74 5-2 未來工作 75 參考文獻 76

    [1]https://www.capstoneturbine.com/products/c1000s
    [2]Epstein, A.H., “Millimeter-scale, MEMS Gas Turbine Engines.” ASME Turbo Expo, Atlanta, Georgia, USA, pp.669-696, June, 2003.
    [3]https://ourworldindata.org/grapher/global-fossil-fuel-consumption
    [4]Xiao, G., Yang, T.-F., Liu, H.-L., Ni, D., Ferrari, M., Li, M., Luo, Z., Cen, K., Ni, M., “Recuperator for Micro Gas Turbines: A Review,” Applied Energy, Vol.197, pp.83-89, 2017.
    [5]Treece, B., Vessa, P., McKeirnan, R., “Microturbine Recuperator Manufacturing and Operating Experience,” ASME Turbo Expo, Amsterdam, The Netherlands, pp.1017-1023, June, 2002.
    [6]洪偉稜, 高轉速渦輪發電系統之設計與驗證研究,國立成功大學航空太空工程系碩士論文,2012年6月。
    [7]張維庭, 微型渦輪發電系統之動力流路設計及分析研究,國立成功大學航空太空工程系碩士論文,2018年7月。
    [8]Giorgettia, S., Parentea, A., Bricteuxc, L., Continob, F., De Paepea, W., “Carbon Clean Combined Heat and Power Production from micro Gas Turbines: Thermodynamic Analysis of Different Scenarios,” Applied Energy, Vol.142, pp.1622-1628, 2017.
    [9]McDonald, C.F., “Recuperator Considerations for Future Higher Efficiency Microturbines,” Applied Thermal Engineering, Vol.2, pp.1463-1487, 1998.
    [10]Kurzke, J., “Gas Turbine Cycle Design Methodology: A Comparison of Parameter Variation with Numerical Optimization,” ASME, Vol.2, München, Germany, June, 1998.
    [11]Gas Turbine Engine Performance Station Identification and Nomenclature, Aerospace Recommended Practice, SAE ARP 755A, Society of Automotive Engineers, Warrandale, Pennsylvania, 1974.
    [12]https://aviation.stackexchange.com/questions/16177/what-are-the-differences-between-a-helicopter-engine-turboshaft-and-an-aircraf
    [13]廖智群, 微型渦輪發電系統測試與驗證研究,國立成功大學航空太空工程系碩士論文, 2013年6月。
    [14]Manfred, F., “Directly Driven Dynamo Electric Machine-Gas Turbine Generator Structure,” U.S. Patents No.4,253,031, 1981.
    [15]http://www.mhiet.co.jp/en/products/turbocharger/technical/index.html
    [16]http://www.proepowersystems.com/proe90.htm
    [17]https://onlinelibrary.wiley.com/doi/pdf/10.1002/9781118534786.app1

    無法下載圖示 校內:2024-06-27公開
    校外:不公開
    電子論文尚未授權公開,紙本請查館藏目錄
    QR CODE