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研究生: 周怡文
Chou, I Wen
論文名稱: 電子裝置機殼開孔狀況對其內部水平鰭片熱沉自然對流的影響
Natural Convection from Horizontal Rectangular Fin Arrays within Perforated Chassis of an Electronic Device
指導教授: 王訓忠
Wong, Shwin-Chung
口試委員: 許文震
Sheu, Wen-Jenn
簡國祥
Chien, Kuo-Hsiang
學位類別: 碩士
Master
系所名稱: 工學院 - 動力機械工程學系
Department of Power Mechanical Engineering
論文出版年: 2015
畢業學年度: 103
語文別: 中文
論文頁數: 60
中文關鍵詞: 自然對流鰭片熱沉機殼開孔
外文關鍵詞: Natural convection, Heat sink, Chassis perforation
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  • 本研究以數值模擬分析電子產品之外殼開孔情形影響內部水平鰭片熱沉之自然對流散熱效果。由於機殼遮蔽熱空氣上升的影響導致鰭片散熱不易,而將機殼適當地開孔有助於改善其散熱效果。針對CPU熱源假設為等溫且底面積為100 mm × 100 mm的固定熱沉的狀況,本研究模擬不同機殼開孔形式、開孔率以及機殼材料對於鰭片熱沉散熱的影響。先以單一通道找出增加散熱量之幾何變動趨勢後,再針對印刷電路板參與計算與否以及不同機殼材料模擬半個機殼之散熱情形。結果顯示由於受熱氣流趨向熱沉中心區域,開孔位於鰭片中央的上方機殼可使熱空氣較順暢地排出而具有較好的散熱效果。遠離鰭片上方之未開孔檔板具有引導環境空氣至熱源附近的作用,可以使空氣能夠被更有效地加熱。模擬半個機殼計算域時,印刷電路板是否參與計算對於鰭片總散熱量只有小幅影響,其差異低於熱沉與電路板在垂直擺放的狀況。使用塑膠做為機殼材料於水平擺放之機殼內鰭片散熱案例比使用鋁材料做為機殼的案例高出約20%的總散熱量。水平擺放下熱沉的熱傳量皆明顯低於垂直擺放下的熱傳量,當考慮印刷電路板參與熱傳下,塑膠機殼中其比值為0.73,但在鋁合金機殼中其比值降為0.61。


    In this study, the effects of chassis perforation on the natural convection from a horizontal rectangular-fin heat sink have been studied numerically. The parameters include perforation pattern, local and overall opening ratio, and the thermal conductivity of the chassis material. In the first part, single-channel analysis is conducted for various perforation patterns. The results show that when the upper chassis wall is perforated over the middle region of the heat sink, with a single perforation or multiple dispersed perforations, the venting flow can be smooth and fast, yielding effective cooling of the heat sink. In the second part, the computation domain includes a half of the system. The effect of the heat transfer associated with the printed circuit board is found to slightly enhance the natural convection from the heat sink when the system is in the horizontal orientation. But stronger enhancement is displayed in the vertical orientation. When plastic is selected as the chassis material, the total heat flux of the heat sink within it is 20% higher than that of the aluminum alloy chassis in horizontal orientation. The total heat fluxes of the heat sink in a horizontal system are significantly lower than those in a vertical system. For example, the ratio of the total heat flux between two different orientations is 0.73 in a plastic chassis, but it decreases to 0.61 in an aluminum alloy chassis.

    摘要 I Abstract II 致謝 III 目錄 IV 圖表目錄 VII 符號表 X 第一章 緒論 1 1.1研究背景 1 1.2 文獻回顧與基礎原理 3 1.3 研究動機與目的 6 第二章 模型建構與理論基礎 17 2.1 數學模型 17 2.1.1 The Boussinesq Model 17 2.1.2 統御方程式 18 2.2 數值方法 19 2.2.1 速度與壓力求解方式 20 2.2.2 其餘離散化方程式 20 2.2.3 相關參數 21 2.3 模擬參數 21 2.4 流固耦合計算之網格與計算域建立 22 第三章 機殼開孔位置對鰭片熱沉散熱的影響 25 3.1物理模型 25 3.1.1模型幾何 25 3.1.2邊界條件 26 3.2上側機殼單一孔洞 28 3.2.1不同開孔位置的散熱比較 28 3.2.2中央開孔大小的影響 29 3.3上側機殼為分散式多孔洞 30 3.3.1 分散孔洞之單一孔洞大小 (Lp) 31 3.3.2局部開孔率(ηl)與中央對稱面到孔洞最遠距離(Lt)的影響 32 3.3.3總開孔率(ηo)與孔洞分布圖形的影響 33 3.4單一鰭片通道與多鰭片通道之間的模擬差異 35 第四章 機殼材料及印刷電路板對水平鰭片熱沉散熱影響 45 4.1物理模型 45 4.1.1模型幾何 45 4.1.2邊界條件 46 4.2機殼水平與垂直擺放下鰭片熱沉對流熱傳的比較 47 4.3電路印刷版是否參與熱傳對於水平與垂直鰭片熱傳的影響 48 4.4不同機殼材料分別在水平與垂直擺放下對鰭片散熱效益的影響 48 第五章 結論 56 參考文獻 58

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