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研究生:林鴻斌
研究生(外文):Lin, Hung-Pin
論文名稱:溫濕度效應對鋁合金蜂巢板承受彎矩負荷下靜態及疲勞強度影響之研究
論文名稱(外文):Effect of Temperature/Humidity on The Static and Fatigue Strength of Aluminum Honeycomb Sandwich Structure under Bending Loading
指導教授:任貽明
指導教授(外文):Jen, Yi-Ming
學位類別:碩士
校院名稱:中華大學
系所名稱:機械工程學系碩士班
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:2010
畢業學年度:98
語文別:中文
中文關鍵詞:鋁合金蜂巢板黏著劑溫度濕度極限強度疲勞壽命
外文關鍵詞:TemperatureHumidityHoneycomb Sandwich PanelsStatic/Fatigue StrengthDebonding
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在工業界中有越來越多的接合案例使用黏著劑接合方法,而蜂巢板就是一恰當實例,具有高強度、質輕、低成本之優點。但由於其黏著劑屬於高分子聚合物,在對於不同溫濕度環境下黏著劑之機械性質相當敏感,因此本研究針對含有一鋁蜂巢結構與上下面板之鋁合金蜂巢板,利用四點彎矩進行靜態及疲勞強度實驗。實驗部分考量從低溫至高溫高濕之七個不同溫濕度環境,以藉此可幫助瞭解溫濕度效應對鋁合金蜂巢板強度之影響。
本研究首先針對不同溫濕度下進行靜態彎矩實驗,藉此觀察其靜態實驗之結果與破壞模式。結果顯示當溫度越低時,蜂巢板之靜態彎矩強度越高,其破壞模式為面板凹陷;隨著溫濕度上升強度則隨之下降,破壞模式也從面板凹陷轉換成面板與蜂巢結構間之介面脫膠破壞。在疲勞實驗部分,將設定每一個溫濕度環境下之五個適當負荷階進行試驗,負荷階之大小分別設定為靜態極限強度之85%、80%、75%、70%、65%、60%、55%、50%、45%、40%、35%、30%及25%,透過疲勞實驗可得到不同溫濕度之負荷-壽命曲線與破壞模式。其結果顯示溫度越低時,疲勞強度越高;隨著溫濕度上升強度則隨之下降。破壞模式部分則皆為面板與蜂巢結構間之介面脫膠破壞。

To understand the effect of temperature/humidity on the bending strength of aluminum honeycomb sandwich panels, the static and cyclic bending strength of the aluminum honeycomb sandwich panels under various environmental conditions will be experimentally analyzed in this study. According to the response of industrial users, the major cause of the fatigue failure of aluminum honeycomb panels is the adhesive debonding between the panel and the cell core. Furthermore, the local hot-wet environment will reduce the fatigue strength apparently. A systemic analysis on the relation between the temperature/humidity and the strength of the honeycomb sandwich panels is necessary urgently.
In the study, the static and fatigue strengths of the aluminum honeycomb sandwich panels are evaluated experimentally under 7 controlled temperature/humidity conditions. In general, the experimental results show that the static/fatigue strength under low temperature environments is slightly higher to that at room temperature. Moreover, the static/fatigue strength of the honeycomb sandwich panels decreases significantly under high temperature environments compared with that at room temperature and the humidity is found to have moderate effect on the static/fatigue strength of the honeycomb sandwich panels.

中文摘要 I
英文摘要 II
誌 謝 III
目 錄 IV
表目錄 VI
圖目錄 VII
符號說明 X
第一章 序論 1
1-1 引言 1
1-2 研究內容 3
1-3 章節概要 3
第二章 文獻回顧 4
第三章 實驗內容與程序 8
3-1 研究對象 8
3-2 儀器介紹 9
3-3 實驗步驟與內容 10
3-3-1 溫濕度環境設定 10
3-3-2 鋁合金蜂巢板在不同溫濕度環境下之靜態及疲勞強度實驗 11
第四章 目前研究成果 19
4-1 鋁合金蜂巢板承受四點彎矩靜態實驗結果 19
4-1-1 溫度對鋁合金蜂巢板承受四點彎矩靜態極限強度之影響 19
4-1-2 濕度對鋁合金蜂巢板承受四點彎矩靜態極限強度之影響 20
4-2 鋁合金蜂巢板承受四點彎矩疲勞實驗結果 20
4-2-1 溫度對鋁合金蜂巢板承受四點彎矩疲勞壽命之影響 21
4-2-2 濕度對鋁合金蜂巢板承受四點彎矩疲勞壽命之影響 22
第五章 結論 77
參考文獻 79

1. L. J. Gibson, and M. F. Ashby, “Cellular Solids” Cambridge, 1988.
2. G. Shi, and P. Tong, “Equivalent Transverse Shear Stiffness of Honeycomb Cores,” International Journal of Solids and Structures, Vol. 32, Issue 10, pp.1383-1393, May 1995.
3. J. M. Albuquerque, M. F. Vaz, and M. A. Fortes, “Effect of Missing Walls on the Compression Behaviour of Honeycombs,” Scripta Materialia, Vol. 41, Issue 2, pp. 167-174, June 1999.
4. W. Becker, “Closed-Form Analysis of the Thickness Effect of Regular Honeycomb Core Material,” Composite Structures, Vol. 48, Issues 1-3, pp. 67-70, January-March 2000.
5. M. Doyoyo, and D. Mohr, “Microstructural Response of Aluminum Honeycomb to Combined Out-of-Plane Loading,” Mechanics of Materials, Vol. 35, Issue 9, pp. 865-876, September 2003.
6. M. Y. Yang, and J. S. Huang, “Elastic Buckling of Regular Hexagonal Honeycombs with Plateau Borders Under Biaxial Compression,” Composite Structures, Vol. 71, Issue 2, pp. 229-237, November 2005.
7. S. D. Pan, L. Z. Wu, Y. G. Sun, Z. G. Zhou, and J. L. Qu, “Longitudinal Shear Strength and Failure Process of Honeycomb Cores,” Composite Structures, Vol. 72, Issue 1, pp. 42-46, January 2006.
8. F. J. Plantema, “Sandwich Construction,” Wiley, 1966.
9. H. G. Allen, “Analysis and Design of Structural Sandwich Panels,” Oxford, 1969.
10. T. Saito, and R. D. Parbery, “Parameter Identification for Aluminum Honeycomb Sandwich Panels Based on Orthotropic Timoshenko Beam Theory,” Journal of Sound and Vibration, Vol. 208, Issue 2, pp. 271-287, November 1997.
11. H. Zhao, and G. Gary, “Crushing Behaviour of Aluminum Honeycombs under Impact Loading,” International Journal of Impact Engineering, Vol. 21, Issue 10, pp. 827-836, November 1998.
12. F. Meraghni, F. Desrumaux, and M. L. Benzeggagh, “Mechanical Behavior of Cellular Core for Structural Sandwich Panels,” Composites Part A: Applied Science and Manufacturing, Vol. 30, Issue 6, pp. 767-779, June 1999.
13. A. Petras, and M. P. F. Sutcliffe, “Failure Mode Maps for Honeycomb Sandwich Panels,” Composite Structures, Vol. 44, Issue 4, pp. 237-252, April 1999.
14. J. K. Paik, A. K. Thayamball, and G. S. Kim, “The Strength Characteristics of Aluminum Honeycomb Sandwich Panels,” Thin-Walled Structures, Vol. 35, Issue3, pp. 205-231, November 1999.
15. S. M. Lee, and T. K. Tsotsis, “Indentation Failure Behavior of Honeycomb Sandwich Panels,” Composites Science and Technology, Vol. 60, Issue8, pp. 1147-1159, June 2000.
16. A. Ural, A. T. Zehnder, and A. R. Ingraffea, “Fracture Mechanics Approach to Face Sheet Delamination in Honeycomb: Measurement of Energy Release Rate of the Adhesive Bond,” Engineering Fracture Mechanics, Vol. 70, Issue 1, pp. 93-103, January 2003.
17. M. Q. Nguyen, S. S. Jacombs, R. S. Thomson, D. Hachenberg, and M. L. Scott, “Simulation of Impact on Sandwich Structures,” Composite Structures, Vol. 67, Issue 2, pp. 217-227, February 2005.
18. J. S. Huang, and J. Y. Lin, “Fatigue of Cellular Materials,” Acta Materialia, Vol. 44, Issue 1, pp. 289-296, January 1996.
19. M. Burman, and D. Zenkert, “Fatigue of Foam Core Sandwich Beam-1: Undamaged Specimens,” International Journal of Fatigue, Vol. 19, Issue 7, pp. 551-561, October 1997.
20. M. Burman, and D. Zenkert, “Fatigue of Foam Core Sandwich Beam-2: Effect of Initial Damage,” International Journal of Fatigue, Vol. 19, Issue 7, pp. 563-578, October 1997.
21. G. Schaffner, X. E. Guo, M. J. Silva, and L. J. Gibson, “Modelling Fatigue Damage Accumulation in Two-Dimensional Voronoi Honeycombs,” International Journal of Mechanical Sciences, Vol. 42, Issue 4, pp. 645-656, April 2000.
22. A. M. Harte, N. A. Fleck, and M. F. Ashby, “The Fatigue Strength of Sandwich Beams With an Aluminium Alloy Foam Core,” International Journal of Fatigue, Vol. 23, Issue 6, pp. 499-507, July 2001.
23. J. S. Huang, and S. Y. Liu, “Fatigue of Honeycombs Under In-Plane Multiaxial Loads,” Materials Science and Engineering A, Vol. 308, Issues 1-2, pp. 45-52, June 2001.
24. N. Kulkarni, H. Mahfuz, S. Jeelani, and L. A. Carlsson, “Fatigue Crack Growth and Life Prediction of Foam Core Sandwich Composites Under Flexural Loading,” Composite Structures, Vol. 59, Issue 4, pp. 499-505, March 2003.
25. E. W. Andrews, L. J. Gibson and M. F. Ashby, “The creep of cellular solids,” Acta Materialia, Vol. 47, Issue 10, pp. 2853-2863, August 1999.
26. E. W. Andrews, J. S. Huang and L. J. Gibson, “Creep behavior of a closed-cell aluminum foam,” Acta Materialia, Vol. 47, Issue 10, pp. 2927-2935, August 1999.
27. D. R. Veazie, K. R. Robinson, K. Shivakumar, “Effect of the marine environment on the interfacial fracture toughness of PVC core sandwich composites,” Composites: Part B engineering, Vol. 35, Issue 6-8, pp. 461-466, September-December 2004.
28. T. S. Gate, X. Su, F. Abdi, G. M. Odegard and H. M. Herring, “Facesheet delamination of composite sandwich materials at cryogenic temperatures,” Composites Science and Technology, Vol. 66, Issue 14, pp. 2423-2435, November 2006.
29. S. M. Soni, R. F. Gibson and E. O. Ayorinde, “The influence of subzero temperatures on fatigue behavior of composite sandwich structures,” Composites Science and Technology, Vol. 69, Issue 6, pp. 829-838, May 2009.
30. S. Allaoui, Z. Aboura, M. L. Benzeggagh, “Effect of the environmental conditions on the mechanical behaviour of the corrugated cardboard, ”Composites Science and Technology, Vol. 69, Issue 1, pp. 104-110, January 2009.
31. A. Siriruk, D. Penumadu, Y. J. Weitsman, “Effect of the sea environmental on interfacial delamination behavior of polymeric sandwich structures, ”Composites Science and Technology, Vol.69, Issue 6, pp. 821-828, May 2009.
32. ASTM, “Flexure Test of Flat Sandwich Constructions,” C393-62, Annual Book of ASTM Standards, 1980.

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