系統識別號 | U0002-0107201416584600 |
---|---|
DOI | 10.6846/TKU.2014.00023 |
論文名稱(中文) | 考慮尾流及後緣襟翼之風機葉片效能研究 |
論文名稱(英文) | The Effects of Wake Dynamics and Trailing Edge Flap on Wind Turbine Blade |
第三語言論文名稱 | |
校院名稱 | 淡江大學 |
系所名稱(中文) | 航空太空工程學系碩士班 |
系所名稱(英文) | Department of Aerospace Engineering |
外國學位學校名稱 | |
外國學位學院名稱 | |
外國學位研究所名稱 | |
學年度 | 102 |
學期 | 2 |
出版年 | 103 |
研究生(中文) | 邱建智 |
研究生(英文) | Chien-Chih Chiu |
學號 | 601430175 |
學位類別 | 碩士 |
語言別 | 繁體中文 |
第二語言別 | |
口試日期 | 2014-06-20 |
論文頁數 | 66頁 |
口試委員 |
指導教授
-
王怡仁(090730@mail.tku.edu.tw)
委員 - 馮朝剛 委員 - 陳蓉珊 |
關鍵字(中) |
葉片元素理論 Peters動態尾流理論 流固耦合 後緣襟翼 |
關鍵字(英) |
Blade Element Theory Peters Dynamics Wake Theory Fluid-Structure Interaction Trailing Edge Flap(TEF) |
第三語言關鍵字 | |
學科別分類 | |
中文摘要 |
本研究是探討風機葉片附加後緣襟翼並考慮此後緣襟翼的大小及攻角(index angle)對於對於風機葉片產生之推力及根部受力的影響。本文透過ANSYS的參數設定語法APDL (ANSYS Parametric Design Language)及FORTRAN程式的結合,探討結合流場及結構之間耦合的狀況,以及兩者相互影響之後流場對結構實際造成的影響。吾人將做一系列的討論,首先由矩形葉片驗證APDL語法與FORTRAN兩種程式結合的可行性,隨後再討論尾流效應對於矩形葉片之影響,最後將以實際之風機葉片附加此新式設計概念之後緣襟翼,模擬實際之應用情況。其中將對於後緣機翼之span大小、在風機葉片之位置及不同的index angle(TEF的flap angle)對於整片葉片之升力,推力及其對於葉片根部之受力做一具體的分析。 |
英文摘要 |
Wind power devices are now used to produce electricity, and commonly termed wind turbines. Load and performance calculations of wind turbines are usually performed by the Blade-Element/Momentum (BEM) method. However, the wake effects and the wake-blade structure interactions are less considered in most wind turbine analysis. This research studied a dynamic wake and blade interacted wind turbine. The Peters dynamic wake theory was applied. The effects of the wake and the configuration of the modern trailing-edge-flap (TEF) on the wind turbine blade were analyzed. The lift and the stresses distribution on the blade were performed by using semi- analytic and numerical wake theory and the combination with APDL(ANSYS Parametric Design Language) and FORTRAN language method. Some comparisons of the wind turbine blade with several TEF parameters such as TEF span-wise length, mid-span position and index angle were fully discussed. The wind turbine blade thrust and root stresses were also be presented. The wake and the TEF configuration effects on a 5MW turbine blade in the lift distribution and stresses were studied to conclude this research. |
第三語言摘要 | |
論文目次 |
目錄 摘要i Abstract ii 目錄 iii 圖目錄 vi 表目錄 viii 第一章 緒論1 一、1研究動機1 一、2文獻回顧5 一、2.1非穩態流場理論5 一、2.2葉片結構動力理論6 一、2.3一般風機葉片之研究8 一、2.4後緣襟翼之研究8 一、3本文架構12 第二章 前置研究方法 14 二、1 動量理論 (Momentum Theory)14 二、2 葉片元素理論 (Blade Element Theory)15 二、3 離心力理論 (Centrifugal Force Theory)17 二、4 動力尾流理論 (Wake Theory)18 二、4.1 改良之 Peters 尾流理論22 第三章 風機葉片流固耦合分析26 矩形旋翼葉片結構與空氣動力耦合分析26 (A) 材料特性與尺寸26 (B) 使用元素26 (C) 網格化與分段面積27 (D) 離心力方程之建立27 (E) 空氣動力方程之建立28 第四章 結果與討論31 四、1 矩形風機葉片結構與空氣動力耦合APDL驗證31 四、2矩形風機葉片理論分析32 四、3 1KW風機葉片結構與動態尾流耦合分析驗證34 四、4 5MW風機葉片結構與動態尾流耦合分析驗證35 四、5 5MW風機葉片加裝後緣襟翼與動態尾流耦合分析36 四、5.1 尾流之影響 36 四、5.2 流固耦合效應之影響37 四、5.3 考慮尾流效應並加裝TEF之影響38 四、5.4 考慮尾流效應並加裝TEF對風機葉片之氣動力與結構影響 39 第五章 結論49 參考文獻51 附錄一 投稿版論文58 圖目錄 圖一 風力發電機種類 3 圖二 水平軸式風力機 4 圖三 垂直軸式風力機 4 圖四 動量理論示意圖 15 圖五 葉片元素示意圖 17 圖六 誘導流值比較圖 (參考文獻 [22], 前飛率 =0.149)24 圖七 和 的關係圖25 圖八SHELL181元素圖27 圖九 葉片空氣動力示意圖29 圖十 分析流程圖30 圖十一 矩形葉片力平衡圖示32 圖十二 矩形葉片升力曲線圖41 圖十三 葉片變形量圖 41 圖十四 葉片扭轉圖42 圖十五 葉片翼展向旋轉程度圖42 圖十六 上翼面蒙氏應力值圖43 圖十七 下翼面蒙氏應力值圖43 圖十八 1KW葉片升力曲線比較圖 44 圖十九 1KW葉片應力分佈比較圖 44 圖二十 5MW葉片9 m/s升力曲線驗證圖45 圖二十一 5MW葉片11.5 m/s升力曲線驗證圖45 圖二十二 TEF翼展R/6未加尾流之應力圖46 圖二十三 TEF翼展R/6加尾流之應力圖46 圖二十四 葉片加裝與未加TEF之升力曲線比較圖47 圖二十五 葉片是否加裝TEF之應力分佈比較圖47 圖二十六 葉片加裝TEF之示意圖 48 表目錄 表一 諧模數 (m) 及相對所取的模層函數的階數 (r)23 表二 材料特性表26 表三 不同TEF span 之結構分析37 表四 耦合疊代之氣動力及結構數據38 表五 不同TEF參數對葉片之影響 40 |
參考文獻 |
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