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研究生: 皮昆田
Pi, Kun-Tian
論文名稱: 史特林引擎鰭片紋路熱傳增益分析
Analysis of Heat Transfer Enhancement of Stirling Engine Slot Grooves
指導教授: 陳文立
Chen, Wen-lih
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: 2020
畢業學年度: 108
語文別: 中文
論文頁數: 229
中文關鍵詞: 史特林引擎衝擊氣流CFD針狀鰭片阻擋效應
外文關鍵詞: CFD, Stirling engine, Impinging jet, Pin fin, Blockage effect
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  • 本研究以改善γ型史特林引擎的熱傳效益為目的,史特林引擎的上板為冷端而底板為熱端,透過設計不同的針狀鰭片,像是長方形、圓形、菱形、錐形等不同的鰭片,安置在史特林引擎的上板與下板,藉此提升其熱傳增益。為了瞭解上述設計所帶來的物理現象,本研究使用了CD-adapco所開發的數值分析軟體STAR-CCM+來分析史特林引擎的內部流場。在分析流場前,本研究會先進行網格獨立測試與時間獨立測試,並從測試結果中得到適合的網格與時間步數後,再進行絕熱驗證。藉由絕熱驗證所得到的壓力與體積帶入關係式中,來增加使用CFD軟體的可信度。
    模擬結果會以鰭片高度做為區隔分開探討,其分別為圓形、長方形、菱形2mm高頂板與底板針狀鰭片,另一部分為圓形、長方形、菱形、錐形3mm高頂板與底板針狀鰭片。從模擬結果中可發現移氣器與移氣器汽缸的衝擊氣流和管狀再生器的衝擊氣流會撞擊底板及頂板,使氣體能夠更有效率的加熱與冷卻史特林引擎的內部氣體;模擬結果也發現在2mm高底板與頂板針狀鰭片中,圓形2mm高針狀鰭片在轉速60rpm、180rpm、300rpm下都有最好的表現,原因是由於其阻擋效應小,使衝擊氣流撞擊到鰭片能夠更有效率的加熱與冷卻氣體;在3mm高底板與頂板針狀鰭片中,圓形3mm高針狀鰭片在轉速60rpm、180rpm、300rpm下有最好的性能表現,由於其阻擋效應較小,衝擊氣流撞擊到鰭片時能夠使鰭片更充分的加熱與冷卻氣體,進而達到最好的性能,但若綜合性能與成本因素,在所有針狀鰭片設計中,圓形3mm高針狀鰭片會是最好的選擇。

    In this study, the gamma type Stirling engine top plate and bottom plate were
    designed with different pin fin shapes, such as rectangular, circular, diamond,
    and conical, to enhance thermal efficiency. In order to research the physical
    phenomenon accompanied by pin fin in the Stirling engine, this study used
    commercial software STAR-CCM+ to analyze the flow field in the Stirling
    engine. Before analyzing the flow field, the first validation was to conduct
    the grid-independent test and the time-step independent test and obtain the
    appropriate mesh and time-step for numerical analysis; then, the second
    validation was to make all walls of the Stirling engine set in an adiabatic
    process. According to the aforementioned steps, the validation showed that
    pressure(p) and volume(V) would follow the theoretical relation of
    pV1.4 = C , and could prove the accuracy of the current CFD approach. The
    simulation results would be discussed separately with different pin fin height
    as the segment. There are circular, rectangular, and diamond in 2mm height
    pin fin in Stirling engine top plate and bottom plate, and the other apart are
    circular, rectangular, diamond, and conical shapes in 3mm height pin fin in
    Stirling engine top plate and bottom plate. It could be found that impinging
    jets were created by the displacer gap channel and regenerator tube, and made
    the heat exchange in the Stirling engine more efficient. The result also found
    among the 2mm height pin fin, circular pin fin have the best performance,
    due to the smallest blockage effect, on the other hand, among the 3mm height
    pin fin circular pin fin have the best performance, due to smallest blockage
    effect. However, considering the cost and feasibility, circular shape pin fin in
    3mm height will be the best option to use.

    目錄 摘要 I Extended Abstract III 誌謝 IX 目錄 X 表目錄 XIII 圖目錄 XIV 符號索引 XXX 第一章、緒論 1 1.1研究背景 3 1.2文獻回顧 6 1.3研究目的與動機 23 第二章、史特林引擎與數值理論探討及應用 24 2.1雷諾平均奈維爾史托克方程式(RANS) 24 2.2紊流模型 26 2.2.1 k-ε雙方程式模型 26 2.2.2 Realizable Two-Layer k-ε紊流模型 28 2.3 史特林引擎基礎理論 32 2.4史特林引擎循環之熱力學理論 34 2.5史特林引擎形式 39 第三章、數值方法設計與模擬 43 3.1數學模型建立 43 3.2幾何模型設計 45 3.3計算域和邊界條件設定 51 3.3.1史特林引擎模擬 51 3.4網格產生 53 第四章、結果與討論 64 4.1網格獨立測試 64 4.2時間獨立性測試 64 4.3絕熱循環驗證 65 4.4史特林引擎模擬結果與分析 66 4.4.1高度2mm針狀鰭片 66 4.4.2高度3mm針狀鰭片 69 4.5 CFD模擬結果與分析 75 4.5.1轉速60rpm各構型2mm底板針狀鰭片物理現象探討 79 4.5.2轉速60rpm各構型3mm底板針狀鰭片物理現象探討 92 4.5.3轉速180rpm各構型2mm底板針狀鰭片物理現象探討 107 4.5.4轉速180rpm各構型3mm底板針狀鰭片物理現象探討 119 4.5.5轉速300rpm各構型2mm底板針狀鰭片物理現象探討 134 4.5.6轉速300rpm各構型3mm底板針狀鰭片物理現象探討 142 4.5.7轉速60rpm各構型2mm頂板針狀鰭片物理現象探討 151 4.5.8轉速60rpm各構型3mm頂板針狀鰭片物理現象探討 163 4.5.9轉速180rpm各構型2mm頂板針狀鰭片物理現象探討 177 4.5.10轉速180rpm各構型3mm頂板針狀鰭片物理現象探討 188 4.5.11轉速300rpm各構型2mm頂板針狀鰭片物理現象探討 201 4.5.12轉速300rpm各構型3mm頂板針狀鰭片物理現象探討 209 4.5.13各轉速下圓型3mm針狀鰭片物理現象探討 218 第五章、結論與未來展望 221 5.1結論 221 5.2未來展望 223 參考文獻 224

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