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研究生: 洪國泰
Kuo-Tai Hung
論文名稱: 小型軸流風扇之設計、模擬與實驗整合研究
An Integrated Numerical and Experimental Study on the Design of Small Axial Flow Fans
指導教授: 林顯群
Sheam-Chyun Lin
口試委員: 郭鴻森
Hong-Sen Kou
陳呈芳
none
學位類別: 碩士
Master
系所名稱: 工程學院 - 機械工程系
Department of Mechanical Engineering
論文出版年: 2007
畢業學年度: 95
語文別: 中文
論文頁數: 267
中文關鍵詞: 葉柵理論扇葉設計渦流設計軸流扇
外文關鍵詞: CFD, axial flow fan, Vortex Design, Cascade
相關次數: 點閱:226下載:15
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中文摘要
本文的目的在建立一軸流風扇的設計流程,而此設計流程只要輸入風扇的設計條件,然後經由簡單的設定即可獲得符合需求的風扇,最後再將設計完成的風扇葉片輸出成三維幾何座標檔,然後藉由電腦輔助設計軟體讀取此幾何檔案,便能夠建構成風扇實體。在設計風扇之前,礙於現有的翼形氣動資料皆僅適用於高雷諾數,而且資料散亂不完整,因此本文藉由數值模擬計算建構一組適用於小型風扇的翼形氣動資料以供設計所需。設計風扇時首先將三維的軸流風扇沿徑向切割成數個二維平面,並分別設定截面的軸向速度與揚程分佈,經由求解速度三角形之後即可獲得所有截面的安裝角與攻角;最後在決定截面的翼形與弦長時,會利用理論推導所得的關係式計算合適與否,當所有截面都挑選完成後即完成設計。在本研究當中將設計所得的結果利用符合AMCA 210-99規範所設計的實驗設備進行驗證,實驗結果比設計目標還要大31%,雖然實驗結果顯示本文的設計方法較保守,但如何減少兩者之間的差距將是日後的研究方向。在本文中所有的計算與設定過程利用Visual Basic撰寫成為應用程式,如此一來便能夠大幅縮短風扇的設計流程,相信此風扇設計程式的完成,將能夠提供風扇的開發人員一套快速且可靠的工具。


Abstract
This research intends to establish a systematic design scheme for small axial-flow fans. First of all, a new low-Reynolds-number database for NACA airfoils is generated via CFD calculations to compensate the shortcoming caused by the present unsuitable airfoil database, which is only valid for high speed flow. The design procedure starts from dividing the 3D rotor blade into several 2D blade shapes uniformly distributed from hub to blade tip. With the assigned axial velocity and head distributions, the attack and setting angles for each 2D blade section can be decided via solving the velocity triangles within the framework of cascade theory. Later, by selecting the airfoil type and chord length, the checking process is performed iteratively to make sure the fulfillment of performance requirement. Thus, the complete rotor is furnished by combining the above 2D blade shapes. Consequently, with the inputs of operating conditions and few settings, this design software, coded by Visual Basic, can generate a fan configuration to meet the requirement and a CAD/CAM file for prototype fabrication. To validate this design tool, a 120mm×120mm×38mm fan is designed using this code and manufactured by the CNC machine to carry out the corresponding experimental verifications. To ensure a reliable outcome, the fan performance test is executed in the AMCA-210 chamber. The experimental and numerical result shows a higher pressure than design target by 31% and 33%, respectively. In conclusion, a conservative, systematic, and user-friendly design tool is established in this study. Hence, design engineer can achieve the required design for small axial-flow fans in a relatively short period and reliable way.

目錄 中文摘要 I Abstract II 致 謝 III 目錄 IV 圖索引 VIII 表索引 XIII 符號索引 XIV 第一章 緒論 1 1.1 前言 1 1.2 文獻回顧 5 1.2.1 風扇設計 7 1.2.2 性能改善 13 1.2.3 數值方法 19 1.3 研究動機與方法 24 1.4 本文大綱 26 第二章 風扇設計 30 2.1 扇葉理論 30 2.1.1 流體對靜止翼列的作用 30 2.1.2 移動翼列對流體的作用 37 2.1.3 無摩擦阻力之葉片計算 41 2.1.4 含摩擦阻力之葉片計算 45 2.2 軸流風扇設計流程 48 第三章 數值方法 69 3.1 統御方程式 69 3.2 紊流與紊流模式 71 3.2.1 紊流 72 3.2.2 紊流模式 79 3.2.3 壁面函數 83 3.3 邊界條件 87 3.4 數值計算方法 91 3.4.1 求解流程 91 3.4.2 離散方法 94 3.4.3 速度與壓力耦合 104 第四章 翼形分析 108 4.1 翼剖面參數 109 4.2 網格建立與數值方法 119 4.3 數值程式驗證 126 4.3.1 網格數驗證 126 4.3.2 模擬與實驗驗證 131 4.4 分析結果 139 第五章 物理模型與數值模型 142 5.1 風扇設計範例 143 5.2 數值模型建立 159 5.2.1 網格建立 159 5.2.2 邊界條件 172 5.2.3 紊流模式與求解設定 174 第六章 數值分析結果 175 6.1 網格獨立性測試 175 6.2 數值結果與誤差分析 179 6.2.1 軸向速度之影響 189 6.2.2 切線速度之影響 196 6.2.3 徑向速度之影響 199 6.3 風扇性能分析 204 第七章 風扇測試 217 7.1 風扇量測設備及儀器 217 7.1.1 風扇性能量測設備 217 7.1.2 噪音量測設備與環境 219 7.2 實驗結果與分析 225 第八章 結論與建議 233 8.1 結論 233 8.2 建議 235 參考文獻 237 作者簡介 246

參考文獻
[1] http://www.tomshardware.com/2005/11/21/the_mother_of_all_cpu_charts_2005/
[2] 陳世雄,動力渦輪機組規劃設計,工研院研究計畫報告(1995)。
[3] Eck, B., “Fans: Design and Operation of Centrifugal, Axial-Flow, and Cross-Flow Fans”, Pergamon Press, New York (1973)
[4] Shepherd, D. G., “Principles of Turbomachinery”, Macmillan Publishing CO., Inc., New York (1956).
[5] 押田良輝,”送風機技術讀本”,復興出版社 (1979)。
[6] Wallis, R. A., “Axial Flow Fans & Ducts”, John Wiley & Sons, Inc., New York (1983).
[7] Horlock, J. H., “Axial flow Compressors”, Krieger (1973).
[8] 聶能光、李福忠,“風機節能與降噪”,科學出版社 (1990) 。
[9] 林國楨,“汽車引擎冷卻風扇設計發展”,機械工業雜誌,民國八十年九月,pp. 204-214。
[10] 簡煥然、施銘銓,“軸流風扇性能測試技術與扇葉技術”,機械工業雜誌,民國八十一年八月,pp. 269-288 。
[11] 施銘銓,“小型冷卻風扇開發介紹”,機械工業雜誌,民國八十四年五月,pp. 148-156。
[12] 張瑞釗、許福忠、施良璘、張起領,“渦輪葉片參數設計法”,中山科學研究院第一研究所研究報告,民國七十五年六月。
[13] 許文英、陳世雄,“軸流式渦輪葉片參數設計”,中國航空太空學會第三十七界學術研討會論文集 (1995)。
[14] 蘇聖斌、陳世雄,“軸流泵葉輪與導葉之設計分析”,中國機械工程學會第十三屆全國學術研討會論文集 ,pp. 298-306 (1996)。
[15] 林至遠,“軸流風扇的性能提昇與測試”,國立成功大學航空太空研究所碩士論文 (1997)。
[16] 林育洲,“軸流風扇之數值與實驗分析”,國立台灣科技大學機械工程系碩士論文 (1998)。
[17] 簡宏斌,“PC風扇之三維數值模擬分析”,國立台灣科技大學機械工程系碩士論文 (1999)。
[18] 林鴻志,“Pentium 4 處理器冷卻風扇之製造與實驗研究”,國立台灣科技大學機械工程系碩士論文 (1999)。
[19] Santos, L. C. and Sankar L.N., “Inverse Design of Aerodynamic Shapes at High Speed Flow”, AIAA paper 94-0090 (1994).
[20] Dang, T. and Isgro, V., “Euler-Based Inverse Method for Turbomechine Blades Part1: Two-Dimensional Cascades”, AIAA Journal, Vol.33, No.12, pp. 2309-2315 (1995).
[21] Damle, S., and Dang, T. “Practical Use of Three-Dimensional Inverse Method for Compressor Blade Design”, ASME Journal of Turbomachinery, Vol. 121, pp. 321-325 (1999).
[22] Nerurkar, A. C., Dang, T. Q., Reddy, E. S., and Reddy, D. R., “Design Study of Turbomachinery Blade by Optimization and Inverse Techniques”, AIAA-96-2555, Lafe Buena Vista, FL (1996).
[23] Pierret, S., and Van den Braembussche, R. A., “Turbomachinery Blade Design Using a Navier-Stokes Solver and Artificial Neural Network”, ASME Journal of Turbomachinery, Vol. 121, No. 2, pp. 326-332 (1998).
[24] Obayashi, S., and Takanashi, S., “Genetic Optimization of Target Pressure Distributions for Inverse Design Methods”, AIAA Journal, Vol. 34, No. 5, pp. 881-886 (1996).
[25] Lewis, R. I., “Turbomachinery Performance Analysis”, John Wiley & Sons, Inc., New York (1996).
[26] Downie, R. J., Thompson, M. C. and Wallis, R. A., “An Engineering Approach to Blade Design for Low to Medium Pressure Rise Rotor-Only Axial Fans”, Experimental Thermal and Fluid Science, Vol. 6, No. 4, pp. 376-401 (1993).
[27] Vad, J., “Three-dimensional flow in axial flow fans of non-free vortex design”, International Journal of Heat and Flow, Vol. 19, No. 6, pp.601-607 (1998).
[28] Sorensen, D. N., “Minimizing The Trailing Edge Noise From Rotor-Only Axial Fans Using Design Optimization”, Journal of Sound and Vibration, Vol. 247, No. 2, pp. 305-323(2001).
[29] Kodama, Y. and Fukano, T., “Flow Characteristics of the Sound Pressure Level and its Prediction for a Low Pressure Axial Flow Fan”, 日本機械學會論文集,53卷492號,pp. 2514-2520(1987)。
[30] Longhouse, R.E., “Vortex Shedding Noise of Low Tip Speed, Axial Flow Fans”, Journal of Sound and Vibration, Vol. 53, No.1, 1997, pp.25-46.
[31] 林顯群,”軸流風扇之性能及噪音分析”,中國航空太空學會第四十屆學術研討會,上冊,pp.87-94(1998)。
[32] Katagiri, H., Fujikake, K. and Yamada, K., “Automotive Mixed Flow Fan with Guide Vanes on Blade Surfaces”, SAE Preprints, 1980, 17p
[33] Kaneko, K., Setoguchi, T.,Nakano, T. and Inoue, M., “Effect of Blade Surface Roughness on Performances of Axial Flow Fans with Different Blade Cambers” , Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan, Vol.50, No. 459, 1984, pp.2812-2817.
[34] Gbadebo, S. A., Hynes, T. P. and Cumpsty, N. A., “Influence of Surface Roughness on Three-Dimensional Separation in Axial Compressors”, ASME Journal of Turbomachinery, Vol.126, Oct. 2004, pp.455-463.
[35] 陳文亮,”小型冷卻風扇之性能與噪音改善研究”,國立台灣科技大學機械工程技術研究所碩士論文,1998年。
[36] Lee, G.H., Baek, J.H. and Myung, H.J., “Structure of Tip Leakage Flow in a Forward-Swept Axial-Flow Fan” , Journal of Flow, Turbulence and Combustion, Vol.70, No.1-4, 2003, pp.241-265.
[37] Nurzia, F. and Puddu, P.,”Experimental Investigation of Secondary Flows in a Low Hub-Tip ratio Fan”, ASME paper, No. 94-GT-377(1994).
[38] Puddu, P., “Tip Leakage Flow Characteristic Downstream of an Axial Flow Fan,” ASME paper, No. 96-GT-508 (1996).
[39] Hideo, F. and Hiroyuki, T. “A Study on Configurations of Casing Treatment For Axial Flow Compressors”, Nippon Kikai Gakkai Ronbunshu, B Hen/Transaction of The Japan, Vol.49, No.448, 1983, pp.2945-2953.
[40] Kawaguchi, K. and Matsui, K., ” Flow Visualization Around Axial Flow Fan Blades” ,Bulletin of the JSME, Vol. 29, No. 248, Feb, 1986, pp. 466-475.
[41] Fukano,T.,Yakamatus,Y., ”The Effects of Tip Clearance on The Noise of Low Pressure Axial And Mixed Flow Fans”, Journal of Sound and Vibration, Vol.105, No.2, 1986, pp.291-308.
[42] Miyake, Y., Inaba, T., and Nishikawa, Y., "A Study on the Flow within the Flow Passage of an Axial Flow Fan Equipped with Air-Separator," Bulletin of JSME, Vol.29, No. 256, No. 256-23, Oct. 1986, pp. 3394-3401.
[43] Inoue, M., Kuroumaru, M., and Ando, Y., “Tip Clearance Flow In Axial Flow Impellers at Low Flow Rate”, Nippon Kikai Gakkai Ronbunshu, B Hen/Transaction of The Japan, Vol.56, No.526, 1990, pp.1960-1965.
[44] Venter, S. J. and Kroger, D. G., “The Effect of Tip Clearance on The Performance of an Axial Flow Fan”, Energy Convers. Mgmt, Vol.33, No.2, 1992, pp.89-97.
[45] 胡文聰,“渦輪機壁層流之實驗與計算研究”,台灣大學應用力學研究所,1994年。
[46] 施尚融,”葉頂間隙對壓縮機性能之影響”,成功大學航空太空工程研究所,2002年。
[47] Hanson, D.B., "Compressible Helicoidal Surface Theory for Propeller Aerodynamics and Noise," AIAA Journal, Vol. 21, No. 6,1983, pp. 881-889.
[48] McFarland, E.R. "Solution of Plane Cascade Flow Using Improved Surface Singularity Methods," Journal of Engineering for Power, Vol. 104, 1982, pp. 668-674.
[49] Woodward, F.A. "An Improved Method for the Aerodynamic Analysis of Wing-Body-Tail Configurations in Subsonic and Supersonic Flows, Part I : Theory and Application," NASA CR-2228,1973.
[50] Kobayakawa, M. and Onuma, H., "Propeller Aerodynamic Performance by Vortex-Lattice Method," Journal of Aircraft, Vol. 22, No. 8, August 1985, pp. 649-654.
[51] Chen, T., Suciu, E.O. and Morino, L., "A Finite Element Method for Potential Aerodynamics around Complex Configurations, "AIAA paper, January 1974.
[52] Chen, S.H. and Williams, M.H., "Panel Method for Counter-Rotating Propfans," Journal of Propulsion and Power, Vol.7,No. 4, July-August 1991.
[53] 孟德化,"軸流式風扇葉片設計",國立成功大學航空太空工程研究所碩士論文,1995 年。
[54] 江易儒,"導管風扇之流場分析",國立成功大學航空太空研究所碩士論文,1996 年。
[55] 張裕慶,"軸流風扇之數值模擬",國立台灣科技大學機械工程技術研究所碩士論文,1997 年。
[56] Wu, C. H., "A General Theory of Three-Dimentional Flow in Subsonic and Supersonic Turbomachines of Axial-, Radial-, and Mixed Flow Type," NACA TN2604, 1952.
[57] Hirsch, C. H. and Warzee, G., "A Finite-Element Method for Through Flow Calculations in Turbomachines," Journal of Fluids Engineering, Trans. ASME, Vol. 98, 1976, pp. 403-421
[58] Arnone, A.,“ Viscous Analysis of Three-Dimensional Rotor Flows Using a Multigrid Method”, NASA TM-106266, 1993.
[59] Chand, K.K. and Lee, K.D., “Turbomachinery Blade Optimization Using the Navier-Stokes Equations”, AIAA Paper 98-0933, 36th Aerospace Sciences Meeting & Exhibit, Reno, NV, January 1998.
[60] Amano, R.S. and Cheng, X.C., “Aerodynamic Blade Optimal Design Of Turbomachinery”, Proceedings of the International Gas Turbine Congress 2003 Tokyo, November 2-7, 2003.
[61] Oro, F.J., Diaz, K.A., Morros, C.S., and Tajadura, R.B., ” Unsteady Flow Analysis of The Stator-Rotor Interaction in an Axial Flow Fan”, Proceedings of ASME FEDSM’03 4th ASME_JSME Joint Fluids Engineering Conference Honolulu, Hawaii, USA, July 6-10, 2003.
[62] Kokturk, T.,” Design And Performance Analysis of a Reversible Axial Flow Fan”, M.S. Thesis, Middle East Technical University, February 1981.
[63] Elhadi, E.E. and Wu, K., “Study of Tip Vortex in Open Axial Flow Fan Using CFD and PIV Techniques ”, 4th Int. Conf. on Heat Transfer, Fluid Mechanics and Thermodynamics (HEFAT2005), Egypt, Sept. 2005.
[64] 游裕傑,“離心式電腦風扇的設計與分析”,國立成功大學機械工程研究所碩士論文,2002 年。
[65] 許豐麟,”新式筆記型電腦冷卻風扇之數值模擬”,國立台灣科技大學機械工程技術研究所碩士論文,2000年。
[66] 黃家烈,”筆記型電腦散熱風扇之研究”,國立台灣科技大學機械工程技術研究所碩士論文,2001年。
[67] 周建安,”小型冷卻風扇在不同流阻下之性能研究”,國立台灣科技大學機械工程技術研究所碩士論文,2004年。
[68] Fluent 6.2 Documentation, FLUENT INC.
[69] Abbott, I.H. and Von Doenhoff, A.E. ,”Theory of Wing Sections”, Dover Publications, New York(1949).
[70] ANSI/AMCA Standard 210-99 (ANSI/ASHRAE 51-1999), “Laboratory Method of Testing Fans for Aerodynamic Performance Rating”, Air Movement and Control Association, Inc., 1999.
[71] ISO-9614-1, “Acoustics-Determination of Sound Power Level of Noise Sources Using Sound Intensity-Part 1: Measurement at Discrete”, 1993(E).
[72] CNS 8753, “Determination of Sound Power Level of Noises for Fan, Blower, and Compressors”, Chinese National Standard, 1982.
[73] ISO-3745, “Acoustics – Determination of Sound Power Levels of Noise Sources Using Sound Pressure – Precision Methods for Anechoic and Hemi-Anechoic Rooms”, 2003.

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