§ 瀏覽學位論文書目資料
  
系統識別號 U0002-0808201311355400
DOI 10.6846/TKU.2013.00239
論文名稱(中文) 史特靈引擎之模擬與設計
論文名稱(英文) Simulation and design of a Stirling engine
第三語言論文名稱
校院名稱 淡江大學
系所名稱(中文) 化學工程與材料工程學系碩士班
系所名稱(英文) Department of Chemical and Materials 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 101
學期 2
出版年 102
研究生(中文) 陳宗成
研究生(英文) Zong-Cheng Chen
學號 600400674
學位類別 碩士
語言別 繁體中文
第二語言別
口試日期 2013-07-22
論文頁數 114頁
口試委員 指導教授 - 張煖
委員 - 程學恆
委員 - 陳錫仁
關鍵字(中) 史特靈引擎
節點模式
有限差分理論
再生器
曲柄滑件機構
關鍵字(英) Stirling engine
Nodal model
Finite difference theory
Regenerator
Slider-crank mechanism
第三語言關鍵字
學科別分類
中文摘要
本論文提出一個以柴油引擎為基礎的alpha型空氣史特靈引擎之基本設計,引擎之熱源來自太陽能集光碟之輻射熱,冷端則使用冷卻水移除熱量,引擎內部設計使用具鰭片之平板構成通道的加熱器、由平板構成通道的冷卻器、以及由篩網與篩網間通道構成的再生器。本研究建立了引擎之三階模式,並與滑動結構曲柄的動力模式連結。引擎內部模式針對加熱器、再生器、冷卻器與冷、熱汽缸求解各節點之動量、質量與能量守恆方程式。
基本個案之分析顯示引擎操作於0.58-1.17 MPa,最大壓差約為0.1 MPa,工作流體溫度介於290-1200 K,再生器內部金屬溫度呈線性分佈,且效能達82.6%。引擎對外輸出功率為0.6 kW,熱效率為12.5%。
本論文分析了六個變更設計方案,包括調整冷卻器與再熱器之尺寸、調整冷卻水之溫度與流量,以及調整工作流體之質量,結果顯示縮小冷卻器可產生最大改善效果,可使引擎對外作功提高為0.8 kW,熱效率可達14.29%。
英文摘要
In this study, a basic design is proposed for an alpha-type hot air Stirling engine developed from a diesel engine. The engine is designed to be heated by the solar radiation from a concentrated solar collector and cooled by cooling water. The gas flow channels in the heater and cooler are constructed by finned and non-finned parallel metal plates, respectively. The regenerator design uses parallel wire screens. 
A third order model for the Stirling engine and a kinematic model for the slider- crank structure are developed and the two models are interconnected to simulate the operation of the whole Stirling engine. The Stirling engine model solves the mass, momentum and energy conservation equations for each control volume or node of the heater, cooler, regenerator and the hot and cold cylinders.

The simulation of the base design case reveals the cyclic operating conditions of the working gas and the solid temperatures. For the gas, the pressure ranged 0.58-1.17 MPa, the maximum pressure difference in the engine is about 0.1 MPa and the temperature ranged 290-1200 K. For the metal in the regenerator, the temperature distribution is linear and the effectiveness of the regenerator is 82.6%. The power output from the engine is 0.6 kW and the thermal efficiency is 12.5%.

In this study, six modified design cases are analyzed, including the adjustment of cooler size, heater size, cooling water temperature, cooling water flow rate and mass of working gas. The simulation results indicate that reducing the size of cooler provides the maximum improvement. The power output and the thermal efficiency can be raised to 0.8 kW and 14.29%., respectively.
第三語言摘要
論文目次
中文摘要	I
英文摘要	II
目錄	III
圖目錄	V
表目錄	VIII
第一章	緒論	1
1.1	研究背景	1
1.2	研究動機與範疇	3
1.3	論文組織與架構	4
第二章	文獻回顧	5
2.1	史特靈引擎	5
2.2	太陽能史特靈引擎	8
2.3	史特靈引擎系統模式	10
第三章	引擎基本設計	14
3.1	史特靈引擎基本類型	14
3.2	史特靈引擎設計	18
3.2.1	加熱器	19
3.2.2	再生器	21
3.2.3	冷卻器	22
3.2.4	曲柄系統	25
第四章	模式建立	28
4.1	引擎節點模式	28
4.1.1	膨脹空間	31
4.1.2	加熱器	32
4.1.3	再生器	35
4.1.4	冷卻器	37
4.1.5	壓縮空間	40
4.2	曲柄動力模式	42
4.3	物理與輸送性質	48
4.3.1	黏度	48
4.3.2	比熱	48
4.3.3	熱傳導係數	49
4.3.4	熱對流係數	49
4.3.5	摩擦因子	50
4.4	模式求解	50
第五章	基本個案分析	52
5.1	史特靈引擎與曲柄結合系統說明	52
5.2	工作流體狀態特性	56
5.3	金屬狀態特性	66
5.4	系統能量分析	70
第六章	最佳化設計分析	79
6.1	變更設計方案	79
6.2	替代設計方案性能分析	89
第七章	結論與建議	103
符號說明	105
參考文獻	110
圖目錄
圖1.1集光型太陽能史特靈引擎電力系統	3
圖2.1史特靈引擎之PV與TS圖	11
圖3.1α型史特靈引擎之結構	15
圖3.2α型史特靈引擎之作動	16
圖3.3β型史特靈引擎之結構	17
圖3.4β型史特靈引擎之作動	17
圖3.5γ型史特靈引擎之結構	18
圖3.6加熱器內部結構	20
圖3.7 再生器內部結構	22
圖3.8冷卻器	24
圖3.9曲柄結構	27
圖4.1 史特靈引擎系統節點	30
圖4.2 膨脹空間節點示意圖	31
圖4.3 加熱器單一節點示意圖	33
圖4.4 再生器單一節點示意圖	36
圖4.5 冷卻器通道側面圖	38
圖4.6 冷卻器單一節點示意圖	38
圖4.7 壓縮空間單一節點示意圖	41
圖4.8 曲柄系統	42
圖4.9 活塞受力	45
圖4.10 連接桿受力	46
圖4.11 曲柄軸受力	47
圖5.1史特靈引擎與曲柄結合系統	53
圖5.2工作流體體積之循環變化	57
圖5.3工作流體壓力之循環變化	57
圖5.4膨脹空間與壓縮空間壓力之循環變化	58
圖5.5工作流體壓力差之循環變化	58
圖5.6工作流體質量之循環變化	59
圖5.7工作流體質量流率之循環變化	60
圖5.8工作流體雷諾數之循環變化	60
圖5.9系統內氣體粒子運動軌跡	61
圖5.10工作流體溫度之循環變化	62
圖5.11冷側工作流體與冷卻流體出口溫度之循環變化	63
圖5.12再生器工作流體溫度之循環變化	64
圖5.13熱側工作流體溫度之循環變化	64
圖5.14工作流體溫度差分佈	65
圖5.15系統內部金屬溫度之循環變化	67
圖5.16系統內部金屬溫度差分佈	67
圖5.17加熱器金屬溫度分佈	68
圖5.18再生器金屬溫度分佈	68
圖5.19冷卻器金屬溫度分佈	69
圖5.20工作流體熱通量與活塞作功之循環變化	71
圖5.21系統週期累積能量	72
圖5.22曲柄力矩之循環變化	73
圖5.23曲柄與飛輪之週期累積功	73
圖5.24模擬過程引擎轉速變化	74
圖5.25穩定運轉之曲柄轉速變化	75
圖5.26膨脹空間與壓縮空間壓力與體積關係	75
圖5.27整體系統壓力與體積關係	76
圖5.28系統能量平衡	77
圖6.1冷卻器設計變更	81
圖6.2加熱器變更設計	85
圖6.3個案1系統能量平衡	91
圖6.4個案2系統能量平衡	93
圖6.5個案3系統能量平衡	95
圖6.6個案4系統能量平衡	97
圖6.7個案5系統能量平衡	99
圖6.8個案6系統能量平衡	101
表目錄
表1.1 太陽產能排行	1
表2.1 不同氣體之相對熱傳特性	7
表5.1 史特靈引擎與曲柄結合系統之裝置尺寸資料	54
表5.2 史特靈引擎與曲柄結合系統之裝置尺寸資料(續)	55
表5.3 基本個案系統性能結果	78
表6.1變更設計列表	79
表6.2個案1變更設計單元尺寸	80
表6.3個案2變更設計單元尺寸	83
表6.4個案3變更設計單元尺寸	87
表6.5個案1系統性能	90
表6.6個案2系統性能	92
表6.7個案3系統性能	94
表6.8個案4系統性能	96
表6.9個案5系統性能	98
表6.10個案6系統性能	100
表6.11設計個案性能比較	102
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