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研究生:李智勝
研究生(外文):Chih-Sheng Li
論文名稱:均質進氣壓燃式引擎之進氣對燃燒特性之效應研究
論文名稱(外文):Effect of Intake on Combustion Characteristics of Homogeneous Charge Compression Ignition Engines
指導教授:吳鴻文吳鴻文引用關係
指導教授(外文):Horng-Wen Wu
學位類別:碩士
校院名稱:國立成功大學
系所名稱:系統及船舶機電工程學系碩博士班
學門:工程學門
學類:機械工程學類
論文種類:學術論文
論文出版年:2006
畢業學年度:94
語文別:中文
論文頁數:152
中文關鍵詞:密閉式循環柴油引擎系統均質壓燃式引擎燃燒性能
外文關鍵詞:homogeneous charge compression ignition engineclose cycle diesel engine systemcombustion performance
相關次數:
  • 被引用被引用:8
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  • 下載下載:50
  • 收藏至我的研究室書目清單書目收藏:0
均質壓燃式引擎(HCCI)可提高DI引擎的熱效率與降低污染物的生成,因均質壓燃式引擎需進採用進氣過程時形成的均質混合氣,所以進行不同預混合比之進氣對均質壓燃式引擎的燃燒性能分析是非常重要的。
本文針對KUBOTA RK-125 型之單缸直噴式柴油引擎進行數值模擬,以KIVA3V-RELEASE2為程式主體,藉由修改程式的進氣組成部份分析在不同引擎轉速下,以不同組成分率之汽油或乙醇與甲醇,進行數值運算分析。並檢視在不同預混合燃氣及組成分率下,進氣歧管處與氣缸內的當量比分佈、引擎熱釋放率、流場與溫度場的情形,並將模擬結果與實驗數據比較。
本研究已成功將柴油引擎之進氣過程導入汽油或乙醇與甲醇的燃氣,並且成功以RNG紊流混合燃燒模式啟動KIVA3V-RELEASE2之化學反應機制。模擬結果顯示汽化熱最高的甲醇進氣燃氣,隨著比例越高會增加缸內吸熱量而提早燃燒造成峰值壓力提高。未來期望本研究的燃燒性能模擬對HCCI引擎安裝在密閉式循環柴油引擎系統 (CCDE系統採用HCCI引擎)時有參考的價值。
The homogeneous charge compression ignition (HCCI) engine can enhance the thermal efficiency of DI engine and reduce the formulation of pollutant. Because the homogeneous charge compression ignition needs to adopt the formation of homogeneous mixture gas in the intake process, it is very important to analyzing the combustion performance of a homogeneous charge compression ignition engine with different intake premixed gas and its contents.
This article is aimed at the KUBOTA RK-125 which is a single cylinder direct injection diesel engine, and carries out the numerical simulation. KIVA3V-RELEASE2 is used as the subject of the program, according to modifying the different intake gas contents in program adopting different proportion of the gasoline, ethanol and methanol under different engine speeds. Also the intake port and in-cylinder distribution of equivalence ratio, heatrelease rate of engine, flow and temperature field are investigated for different intake premixed gas and its contents, and the results between the simulation and the experiment will be compared .
The research has already entered the gasoline, ethanol and methanol successfully in the intake process, and succeed in initialing the chemical reaction mechanism of KIVA3V-RELEASE2 using the RNG model of turbulence mixing combustion. The simulation result show that following proportion being the higher, heat of vaporization supreme methanol occur burn in lower temperature and its pressure peak value will rise because of increasing in-cylinder absorption of heat . The simulation combustion process in this research are expected to be a reference value when the close cycle diesel engine system installs with HCCI engine in the future.
摘要………………………………………………I
Abstract…………………………………………II
致謝………………………………………………IV
目錄………………………………………………V
表目錄…………………………………………VⅢ
圖目錄……………………………………………IX
符號說明…………………………………………XVII
第一章 緒論…………………………………1
1-1 研究目的及背景………………………………………………1
1-2 文獻回顧……………………………………4
1-3 研究方向與貢獻………………………………………………9
第二章 數值方法………………………………………………10
2-1 問題描述………………………………………………10
2-2 系統之假設及邊界條件………………………………………………10
2-3 統御方程式………………………………………………12
2-3.1 氣相統御方程式………………………………………………12
2-3.2 液相統御方程式………………………………………………15
2-4 引擎燃燒模式………………………………………………16
2-4.1 預混合燃氣之當量比計算………………………………17
2-4.2 著火遲延對燃燒影響………………………………18
2-4.3 紊流混合燃燒模式………………………………20
2-5數值方法………………………………………………21
第三章 實驗方法………………………………………………24
3-1 實驗概述………………………………………………24
3-1.1 實驗設備圖………………………………………………24
3-1.2 實驗設備規格………………………………………………25
3-2 輔助燃油燃料特性比較………………………………………………27
3-3 均質進氣壓燃式引擎實驗之數據量測………………………………………………28
3-3.1 曲柄角之量測………………………………28
3-3.2 氣缸壓力之量測………………………………29
3-3.3 轉速、馬力輸出與負載之量測………………………………29
3-3.4 噴油壓力設定與量測………………………………………………29
3-3.5 制動耗油(bsfc)之量測………………………………………………30
3-3.6 輔助預混合燃氣組成濃度計算………………………………………………30
3-4 均質進氣壓燃式引擎的淨熱釋放率計算模式………………………………………………31
3-5實驗步驟………………………………………………35
第四章 結果與討論………………………………………………37
4-1格點系統測試………………………………………………37
4-2擬與實驗之壓力分析與熱釋率比較…………………………………………38
4-3混合燃氣當量比分佈…………………………………………43
4-4不同預混合比之進氣的燃燒模擬…………………………………………44
4-4.1 1800rpm下不同燃氣之預混合比對燃燒性能的效應…45
4-4.2 1500rpm下不同燃氣之預混合比對燃燒性能的效應…47
4-4.3 1200rpm下不同燃氣之預混合比對燃燒性能的效應…49
第五章 結論與未來展望………………………………………………52
5-1 結論………………………………………………52
5-2 未來展望………………………………………………54
參考文獻………………………………………56
自述……………………………………………128
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