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研究生:溫文龍
研究生(外文):Wen-Lung Wen
論文名稱:微型渦輪機發電系統實驗研究
論文名稱(外文):Study of Microturbine Generator System Testing Technology
指導教授:蔣小偉蔣小偉引用關係
指導教授(外文):Hsiao-Wei Chiang
學位類別:碩士
校院名稱:國立清華大學
系所名稱:動力機械工程學系
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:2002
畢業學年度:90
語文別:中文
論文頁數:72
中文關鍵詞:微型渦輪機基線性能引擎熱運轉
外文關鍵詞:microturbinebaseline performanceengine hot testing
相關次數:
  • 被引用被引用:5
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本文對於375hp微型渦輪機發電系統之實驗架構包括引擎進、排氣段、測試基座、操作控制系統及量測系統等有初步之介紹。此外,在操作控制系統方面對於引擎啟動裝置、燃料供應系統、潤滑油供應系統、點火系統及燃燒室二次空氣供給系統等已完成其實驗架構部分,並對引擎基線性能量測所需建立之量測設備和數據擷取系統作了完整規劃與初步建構。而RGT-3600配套系統之引進,除了可建立其測試能量外,並能作為日後實驗架構之電路控制系統與量測訊號接出配置等之參考。
研究中作了引擎試運轉測試,找出引擎點火之最佳條件及引擎熱運轉所遭遇之問題與解決方案。並使用GasTurb分析軟體作了引擎性能分析預測,發現預測結果與引擎之設計點與非設計點性能參數趨勢符合,證明GasTurb分析軟體可作為配備再生系統之微型渦輪機引擎性能分析之可行性,並提供日後性能分析與真正之實驗數據作比對與驗證。
This thesis introduces the experimental foundation for a 375hp microturbine generator system, which includes inlet and exhaust section, testing frame, operating control system and measurement system. Besides, we have set up the operating control system which includes starter system, fuel supply system, lubrication system, ignition system and secondary air supply system of combustor. And we have completely designed and constructed the measurement devices and data acquisition system that are needed for measuring of engine baseline performance. Furthermore, RGT-3600 packaging system not only can establish its testing capacity, but also will provide circuit control system structure and arrangement of signal output hereafter.
In this study, we have done test run of engine and study the best condition of engine starting and study of engine hot testing. We also applied GasTurb software to predict the engine performance. The result revealed the trends of engine design point and off-design point performance parameters which are close to experimental results. This proved that GasTurb software is capable to analyze performance of regenerative microturbine generation system and to compare with experimental data.
中文摘要………………………………………………………………….I
ABSTRACT……………………………………………………………...II
誌謝……………………………………………………………………..III
目錄……………………………………………………………………..IV
表目錄………………………………………………………………….VII
圖目錄…..…………………………………………………………….VIII
符號說明………………………………………………………………..IX
第一章 緒論
1.1引言………………………………………………………...………1
1.2文獻回顧………………………………………………………...…3
1.3研究目的……………………………………………………...……8
第二章 研究方法
2.1 實驗設備……………………...…………………………………9
2.1.1 操作控制系統………………………………………………10
2.1.1.1 啟動裝置……………………………………………10
2.1.1.2 燃料供應系統……………………………………….11
2.1.1.3 潤滑油供應系統…………………………………….12
2.1.1.4 點火系統..…………………………………………….13
2.1.1.5 二次空氣供給系統………………………………….13
2.1.2 RGT-3600引擎配套系統…………………………………13
2.2 量測系統………………………………………….……………..15
2.2.1 量測設備……………………………………………………15
2.2.2 數據擷取系統……………………………………………….18
2.3 實驗方法………………………………………………………19
2.3.1 引擎運轉實驗前置作業……………………………………19
2.3.2 冷運轉實驗操作……………………………………………20
2.3.3 熱運轉(點火)實驗操作……………………………………20
2.3.4 RGT-3600引擎配套系統運轉實驗前置作業……………...21
2.3.5 RGT-3600引擎配套系統運轉實驗操作…………………...21
2.3.6 RGT-3600引擎配套系統停車實驗操作…………………...22
第三章 結果與理論分析
3.1 理論分析………….……….…………………………………..23
3.1.1 問題之描述…………………………………………………23
3.2.2 數學模式……………………………………………………23
3.2 結果與討論……………………….……………………………..25
3.2.1 實驗之結果與討論…………….………………………….25
3.2.2 GasTurb分析預測之結果與討論...…………………………26
第四章 結論與建議
4.1 結論……………………………………………………………27
4.2 建議……………………………………………………………28
參考文獻………………………………………….…………………….29
附 錄……………………………………………………………….61
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