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研究生: 楊翰勳
Yang, Hang-Suin
論文名稱: 熱延遲式史特靈引擎之理論分析與製作
Theoretical Analysis and Manufacturing of a Thermal-Lag Stirling Engine
指導教授: 鄭金祥
Cheng, Chin-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: 2011
畢業學年度: 99
語文別: 中文
論文頁數: 113
中文關鍵詞: 熱延遲式史特靈引擎理論模型
外文關鍵詞: Thermal lag, Stirling engine, Theoretical Model
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  • 本研究探討熱延遲式史特靈引擎的運作原理。先期以模型引擎作為研究基礎,觀察不同操作條件下,引擎之動力性質。後期架構熱延遲式史特靈引擎之熱力與動力模式,模擬引擎性能,並探討引擎起始轉速、飛輪慣量、衝程、缸徑、各部位體積、再生加熱器設計參數、以及熱阻等設計參數對引擎性能的影響。
    研究結果指出,飛輪起始動能的大小對於引擎的運轉狀態有決定性的影響,若起始動能太小,飛輪將進入左右擺盪的狀態或停止,只有當起始動能足夠大,才能使引擎啟動,並穩定運轉。引擎的汽缸缸徑、活塞衝程與各部位體積的搭配相當重要,皆會影響引擎的運轉狀態與性能。再生加熱器的設計尤為重要,除了進行工作流體的再生外,還必須進行工作流體與高溫熱儲之間的熱交換。模擬結果指出,熱效率與機械效率隨引擎運轉速度增加而降低,而引擎存在最佳操作轉速使其軸功最大。藉由理論模式進行參數分析,找出最佳之參數組合,並設計新型引擎,且試運轉成功,引擎轉速可達1600 rpm。

    This study is concerned with the development of numerical model of thermal-lag Stirling engine. Preliminary model engines were manufactured firstly, and some dynamic characteristics at different operating conditions were observed. Thermodynamic and dynamic numerical models were built and combined to study the performance of the engine. Effects of the initial engine speed, the inertial of flywheel, the bore size, the stroke of piston, the volume of working space, the parameter of regenerative heater, and the thermal resistance are investigated.
    Results show that the magnitude of initial kinetic energy of the flywheel will affect the stable operation mode. If the initial kinetic energy of the flywheel is too small, the flywheel may swing back-and-forth or even stop. It is only when the initial kinetic energy of the flywheel is sufficiently high, the engine can be started to reach a stable operation mode. The collocation among the bore size, the stroke of piston, and the volume of working space is critical. It may affect the operation mode and the performance of the engine. The regenerative heater should be carefully designed because the function of the regenerative heater is not only for regeneration, but also for heat exchanging between the working fluid and the thermal reservoir. It is also found that the thermal efficiency and the mechanical efficiency decrease with increasing engine speed. There exists an optimal engine speed for maximum shaft work. A parametric study is performed based on the numerical model so as to determine the optimal combination of the design parameters. A test engine is designed in accordance with the obtained optimal design parameters combination. It is observed that the test engine is operating successfully and the engine speed is able to reach 1600 rpm.

    目錄 摘要 I ABSTRACT II 誌謝 IV 目錄 VI 表目錄 X 圖目錄 XI 符號索引 XIV 第一章 導論 1 1.1 研究動機 1 1.2 史特靈引擎概要 2 1.2.1 發展概要 2 1.2.2 史特靈引擎的應用 2 1.2.3 史特靈引擎的分類 3 1.3 熱延遲式引擎運作原理探討 5 1.3.1 傳統α型史特靈引擎運作原理 5 1.3.2 熱延遲式引擎運作原理 6 1.3.3 熱延遲式史特靈引擎運作原理 7 1.4 研究目的 8 1.5 論文架構 8 第二章 引擎模型設計與製作 10 2.1 熱延遲式史特靈引擎概論 10 2.1.1 啟動方式 10 2.1.2 曲柄機構之運轉特性 10 2.1.3 自由活塞式之運轉特性 11 2.1.4 加熱方式 12 2.1.5 設計參數 12 2.2 曲柄機構熱延遲式史特靈引擎模型 13 2.2.1 機構設計 13 2.2.2 曲柄機構行波熱延遲式史特靈引擎模型 13 2.2.3 曲柄機構駐波熱延遲式史特靈引擎模型 14 2.2.4 行波熱延遲式史特靈引擎與傳統史特零引擎比較 14 2.3 自由活塞熱延遲式史特靈引擎模型 15 2.3.1 機構設計 16 2.3.2 自由活塞行波熱延遲式史特靈引擎模型 16 2.3.3 自由活塞駐波熱延遲式史特靈引擎模型 17 2.4 引擎發展方向 17 第三章 理論模式 19 3.1 幾何參數與初始條件設定 19 3.2 動力模式 23 3.2.1 各部件速度與加速度 23 3.2.2 各部件受力計算 25 3.3 熱力模式 28 3.3.1 質量流率 29 3.3.2 再生加熱器 31 3.3.3 溫度與壓力 33 3.3.4 引擎輸出功率與熱效率 36 第四章 結果與討論 39 4.1 運轉速度與軸功之關係 39 4.2 熱力性質 40 4.3 起始轉速之影響 41 4.4 飛輪慣量的影響 42 4.5 不同氣室壁面溫度的影響 44 4.6 摩擦係數的影響 44 4.7 衝程的影響 44 4.8 汽缸缸徑的影響 45 4.9 汽缸與氣室熱阻的影響 45 4.10 緩衝室熱阻的影響 46 4.11 氣室與緩衝室體積的影響 46 4.12 再生加熱器物理特性的影響 47 4.13 工作區間與背壓區間填充壓力的影響 49 4.14 負載扭矩對引擎轉速的影響 49 4.15 新型熱延遲式史特靈引擎設計與製作 50 第五章 結論 52 參考文獻 54 圖表 57 VITA 112 PUBLICATION LIST 113 表目錄 表4.1引擎基準組之幾何尺寸與操作參數 57 圖目錄 圖1.1 史特靈引擎分類 58 圖1.2史特靈循環p-V圖 60 圖1.3史特靈引擎運作原理示意圖 61 圖1.4 Chen-West與Tailer's熱延遲式引擎概念圖 62 圖1.5 駐波熱延遲式史特靈引擎運作原理圖 63 圖2.1 熱延遲式史特靈引擎分類圖 64 圖2.2 熱延遲式史特靈引擎參數示意圖 65 圖2.3 曲柄機構熱延遲式史特靈引擎模型零件圖 66 圖2.4 曲柄機構行波與駐波熱延遲式史特靈引擎模型 67 圖2.5 α型史特靈引擎與行波熱延遲式史特靈引擎模型 68 圖2.6 自由活塞熱延遲式史特靈引擎模型零件圖 69 圖2.7 自由活塞形波與駐波熱延遲式史特靈引擎模型 70 圖3.1 曲柄機構自由體圖 71 圖3.2 再生加熱器溫度分佈示意圖 72 圖3.3 程式流程圖 73 圖4.1 基準組引擎平均轉速與瞬時轉速對於時間之關係圖 74 圖4.2 基準組指示功、軸功與摩擦功對於時間之關係圖 75 圖4.3 基準組緩衝室與氣室之工作流體質量變化圖 76 圖4.4 基準組緩衝室和氣室之壓力與壓降變化圖 77 圖4.5 基準組緩衝室與氣室之順時溫度與平均溫度變化圖 78 圖4.6 基準組緩衝室、再生加熱器和氣室熱傳與指示功之關係圖 79 圖4.7 基準組p-V圖 80 圖4.8 基準組熱效率隨時間之變化 81 圖4.9 基準組活塞位移、速度與緩衝室壓力之關係圖 82 圖4.10 不同起始轉速對引擎運轉速度之影響 83 圖4.11 低起始轉速對引擎運轉速度之影響 84 圖4.12 低起始轉速對活塞位移變化之影響 85 圖4.13 極低起始轉速對引擎轉速與活塞位移的影響 86 圖4.14 飛輪慣量對引擎轉速的影響 87 圖4.15 低飛輪慣量對引擎轉速的影響 88 圖4.16 臨界轉動慣量對引擎轉速之影響 89 圖4.17 氣室壁面溫度對引擎轉速與指示功之影響 90 圖4.18 摩擦係數對引擎轉速與指示功之影響 91 圖4.19 曲柄軸偏心距對引擎轉速與指示功之影響 92 圖4.20 缸徑對引擎轉速與指示功之影響 93 圖4.21 缸徑對引擎轉速之影響 94 圖4.22 缸徑對活塞振盪之影響 95 圖4.23 熱阻對引擎轉速與指示功之影響 96 圖4.24 增加熱阻對引擎轉速之影響 97 圖4.25 增加熱阻對活塞振盪之影響 98 圖4.26 緩衝室熱阻對引擎轉速與指示功之影響 99 圖4.27 氣室體積對引擎轉速與指示功之影響 100 圖4.28 緩衝室體積對引擎轉速與指示功之影響 101 圖4.29 對引擎轉速與指示功之影響 102 圖4.30 對引擎轉速與指示功之影響 103 圖4.31 再生加熱器孔隙率對引擎轉速與指示功之影響 104 圖4.32 填充壓力對引擎轉速與指示功之影響 105 圖4.33 不同負載對引擎轉速與指示功之影響 106 圖4.34 不同負載扭矩下之p-V圖 107 圖4.35 負載扭矩與轉速之關係圖 108 圖4.36 指示功與軸功對運轉速度之關係圖 109 圖4.37 曲柄機構駐波熱延遲式史特靈引擎之零件圖 110 圖4.38 曲柄機構駐波熱延遲式史特靈引擎實體圖 111

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