藥柱低週疲勞特性與壽限評估模式之研究

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姓名

李耀宗(Yaw-Tzoung Lee) 查詢紙本館藏

畢業系所

機械工程學系

論文名稱

藥柱低週疲勞特性與壽限評估模式之研究

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摘要(中)

本研究探討固體藥柱之低週疲勞性質，以及建立低週疲勞壽限評估方式。除了進行等應變振幅疲勞試驗外，還利用等效之掛載振動頻譜在不同應變水準下進行變動振幅疲勞試驗，以求取疲勞壽限值。在低週疲勞壽限分析中，探討平均應力修正模式及循環計數法之影響，以了解適用於藥柱之低週疲勞壽限評估模式。
本研究求得藥柱之循環應力-應變方程式及應變-壽命方程式。且由研究結果得知當藥柱在掛載頻譜負荷下，以Morrow平均應力修正法搭配雨流區間法進行疲勞壽限分析，可得最佳結果，但若能再加計潛變損傷之影響則更佳。由試件之破斷面觀察發現到，在等應變振幅條件下主要以剝落方式造成損壞，而在變動應變振幅條件則以劈裂方式發生。

摘要(英)

This thesis investigates low cycle fatigue properties and fatigue life prediction model of solid propellant. In addition to the constant strain amplitude fatigue test, the spectrum fatigue test of solid propellant was performed. The present fatigue life prediction model is strain based. Effects of strain ratio (R) and cycle counting method on the predicted life were studied.
The author obtains the cyclic stress-strain equation and strain-life equation of solid propellant in this study. When the solid propellant under spectrum loading, the best fatigue life prediction model is the strain-life model combined Morrow mean stress correction with rainflow histogram cycle counting method. From the analysis of fractographs, it is seen that many solid grains peel off the matrix on facture surface in R= -1 spectrum fatigue test. While the fracture mechanism changes into split in R = 0.5 spectrum fatigue.

關鍵字(中)

★ 壽限預估
★ 固體藥柱
★ 頻譜負荷
★ 平均應力
★ 疲勞

關鍵字(英)

★ mean stress
★ solid propellant
★ fatigue
★ life prediction
★ spectrum loading

論文目次

總目錄
摘要 I
Abstract II
誌謝 III
總目錄 IV
符號說明 VII
圖目錄 IX
表目錄 XII
第一章緒論 1
1-1 研究動機與目的 1
1-2 研究內容 2
1-3 研究架構 2
1-4 文獻回顧 5
1-4-1 藥柱相關研究 5
1-4-2 疲勞相關研究 9
第二章理論說明 14
2-1 應變-疲勞壽限法 14
2-2 循環計數 16
2-3 平均應力修正 20
2-4 次序效應修正 21
2-5 損傷累計 25
第三章研究方法 26
3-1 等應變振幅疲勞試驗 26
3-1-1 實驗設備 26
3-1-2 夾治具設計與試片製作 28
3-1-3 試驗規劃 32
3-2 變動應變振幅疲勞試驗 34
3-2-1 實驗設備 34
3-2-2 夾治具設計與試片製作 34
3-2-3 實驗規劃 35
3-3 破斷面觀察 40
第四章結果與討論 41
4-1 等應變振幅疲勞試驗結果 41
4-2 變動應變振幅疲勞試驗結果 46
4-2-1循環計數法之影響 46
4-2-2 平均應力修正模式之影響 46
4-3 破斷面觀察 53
第五章結論與未來發展 57
參考文獻 58

參考文獻

1 R. Neviere. “An Extension of the Time-Temperature Superposition Principle to Non-linear Viscoelastic Solids”, Int. J. Solids Structures ,“Article in Press. 2005.
2 M. R. Lajczok, “Effective propellant modulus approach for solid rocket motor ignition structural analysis”, Computers & Structures Vol. 56, No.1, July 3, 1995, pp. 101-104.
3 B. Nageswara, “ Fracture toughness of nitramine and composite solid propellants”, Materials Science & Engineering, A Vol.: 403, No.1-2, August 25, 2005, pp. 125-133.
4 M. Shimizu, T. Fujiwara, and K. Ito, “Fatigue of HTPB Composite Solid Propellant and Its Effects on Combustion Properties”, Proc. 13th Int. Symp. on Space Tech. & Sci., Tokyo, pp.167-174, 1982.
5 “Handbook for the Engineering Structural Analysis of Solid Propellant", CPIA-PUB-214.
6 S. Y. Ho, “Viscoelastic Response of Solid Rocket Motor Components for Service Life Assessment”, Journal of Materials Science, Vol. 32, No. 19, pp. 5155-5161, 1997.
7 S. W. Beckwith, “An Integrated Approach to Solid Propellant Cumulative Damage”, Solid Rocket Structural Integrity Abstracts, Vol. 6, No. 3, AFRPL-TR-69-173, July 1969.
8 N. Palazotto , V. Birman., “Environmental and Viscoelastic Effects on stresses in adhesive joints”, Journal of Aerospace Engineering, Vol. 8, No. 2, pp. 107-118, April 1995.
9 R. N. Chappell, F. R. Jensen, and R. W. Burton, “ Statistical Service Life Prediction: Minuteman Third Stage Propellant Grain”, Journal of Spacecraft, Vol. 5, No. 1, 1968.
10 P. W. Davies, W. J. Evans, K. R. Williams, and B. Wilshire, Scripta Met., Vol. 3, pp. 671, 1969.
11 E. J. S. Duncon, J. Margetson, “A Nonlinear Viscoelastic Theory for Solid Rocket Propellants Based on a Cumulative Damage Approach”, Propellants, Explosives, Pyrotechnics, Vol. 23, pp. 94-104, 1998.
12 全湘偉，“飛彈發動機藥柱於超結構試驗之週期估算暨壽限分析模式建立”，新新雙月刊，第廿三卷，第五期，p152~ p165 ，(1995)
13 蘇富湖，卞獨敏，彭匯成，“藥柱壽限研究回顧”，火藥技術，第八卷，第四期，pp.9-15，民國81年。
14 陳正宗，李清國，林立信，“藥柱累積破壞之應用- 壽限預估”，新新季刊，第十七卷，第三期，pp.155-163，民國78年。
15 蔡宜璋，“藥柱結構分析及其在壽限預估的應用簡介”，新新季刊，第十九卷，第三期，pp.63~73，民國80年。
16 全湘偉，“藥柱可壓縮與不可壓縮材料假設對結構力學反應之研究探討”，新新季刊，第三十二卷，第二期，pp.104-115，民國93年。
17 沈盈志，“環境加速壽命試驗規劃與分析”，中華民國第四屆可靠度與維護技術研討會，2001/11/23-24，台北市，pp.369-373，民國90年。
18 沈盈志，王國雄，“掛載振動環境之步進頻譜加速試驗規格擬定方法”，中國航空太空學會學刊，第29卷，第1期，pp.73-80，民國86年。
19 鄒正德，張錫邦，辜文雄，“中空圓柱型藥柱之應力分析” ，火藥技術，第七卷，第二期，pp.23-27，民國80年。
20 全湘偉，"飛彈發動機藥柱結構黏彈材料之力學分析模式建立探討"，新新季刊，第二十四卷，第四期，pp.208~228，民國85年。
21 劉衾瑋，“藥柱疲勞特性與壽限評估模式之研究”，國立中央大學，碩士論文，民國94年7月。
22 K. W. Bills etc.," Accumulative Damage Concept for Propellant-Liner Bonds in Solid Rocket Motors", Journal of Spacecraft, 1987.
23 Wohler, “Uber die Festigkeitversuche mit Eisen und Stahl”,Zeitschrift fur Bauwesen Vol. VIII, X, XIII, XVI, and XX, 1860/70. English Account of this work is in Engineering, Vol. 11, 1871.
24 W. Fairbrain, “Experiments to Determine the Effect of Impact, Vibratory Action, and Long Continued Changes of Load on Wrought Iron Girders”, Philosophical Transactions of the Royal Society, London, 154, 311, 1864.
25 H. Gerber, “Bestimmung der Zulassigen Spannungen in Eisenknostru- ctionen”, Zeitschrift, des Bayerischen Architecjten undIngenieurvereins, Vol. 6, pp.101-110, 1874.
26 J. Goodman, “Mechanics Applied to Engineering, London”, Longmans, Green, 1899.
27 J. Bauchinger, “Ueber die Veranderungen der Elasti zitatsgrenze Erwarman Abkuhlen und durch oftmals wiederholte Belastung”,Mitt: Mech-Tech Lab., XIII Munchen, 1866.
28 H. Basquin, “ The Exponential Law of Endurance Test”, Proceedings of the American Society for Testing and Materials, Vol. 10, pp. 625-630, 1910.
29 H. J. Cough, The Fatigue of Metals, Scott, Greenwood and Son, London, 1926.
30 H. F. Moore, and J. B. Kommers, The Fatigue of Metals, McGraw-Hill Book Co., New York, 1927.
31 S. S. Manson, “Behavior od Materials under Conditions of Thermal Stress”, Heat Transfer Symposium, University of Michigan Engineering Research Institute , 1953 , pp.9-75.
32 L. F. Coffin, “A Study of Effects of Cyclic Thermal Stresses on a Ductile Metal ”, Transactions of the American Society of Mechanical Engineers, Vol. 76, pp. 931-950, 1954.
33 S. S. Manson, “Behavior of Materials under Conditions of Thermal Stress ”, National Advisory Commission on Aeronautics, Report 1170, Cleveland: Lewis Flight Propulsion Laboratory, 1954.
34 J. Morrow, “Fatigue Design Handbook,Advances in Engineering ,Vol. 4 , Society of Automative Engineers ” , Warrendale , Pa. , 1968 , Sec. 3.2 ,p.21-29.
35 K. N. Smith , P. Watson , and T. H. Topper, “A Stress-Strain Function for the fatigue of Metals ” , Journal of Mater. ,Vol. 17 , No. 2 ,1970 , pp 767-778.
36 S. S. Manson and G. R. Halford, “Practical Implementation of Double Linear Damage Rule and Damage Curve Approach for Treating Cumulative Fatigue Damage ”, International Journal of Fracture., Vol. 5 , No. 4 ,1981, pp. 169-172.
37 R. W. Herzberg, “Deformation and Fracture Mechanics of Engineering Materials ”, 2nd ed.. , Wiley , New York ,1983.
38 W. D. Kim , H. J. Lee , J. Y. Kim , S. k. Koh , “ Fatigue Life Estimation of an Engine Rubber Mount”, International Journal of Fatigue Vol. 26, Issue: 5, pp. 553-560, May, 2004.
39 N. Saintier , G. Cailletaud , R. Piques , “Multiaxial Fatigue Life Prediction for a Natural Rubber ”, International Journal of Fatigue, Vol.28 , pp.530-539, 2006.
40 N. Bonora, G. M. Newaz, “Low Cycle Fatigue Estimation for Ductile Metals using a Nonlinear Continuum Damage Mechanics Model” , International Journal of Solids Structures,Vol. 35, No. 16, pp. 1881-1894,1998.
41 Q. Z. Chen, “Research on Fatigue Life of Components Simulatiing Key Structure of a Certain Type Aircraft”, Vol.26(S), pp.222-225, Journal of Mechanical Strength (In China), 2004.
42 C. S. Chang, W. T. Pimbley, H. D. Conway, “An Analysis of Metal Fatigue based on Hysteresis Energy”, Experimental Mechanics, 1968, Vol. 8, No. 3. pp.133-140.
43 D. E. Martin “An Energy Criterion for Low-Cycle Fatigue”, J. Base Engineer, 1931, Vol.81,No.12, pp.565-576.
44 K. Golos, F. Ellyin, “Total Strain Energy Density Theory for Cumulative Fatigue Damage”, J. Pressure Vessel Technology, ASME, 1988, Vol.110, No.1, pp.36-42.
45 H. Harig, K. Muller “Investigation in the Cyclic Deformation Behavior of Notched Steel Specimens by mean of the Thermoelastic effect” Materialprufung, 1986, Vol. 28, No. 11, pp.357-364.
46 M. K. Harig, “Thermometric Investigations of the Damage Process under Single Stage Loading and Simple Program Loading History”, Material Technology and testing,1986, Vol.17, No. 7, pp251-261.
47 R. Vinet, R. Connolly, R. Gauvin,“Temperature Rise in a Thermoplastic under Completely Reversed Bending Stresses”, Polymer Engineering Science, 1981, Vol.21, No.18, pp.1203-1212.
48 S. N. Gu, L. J. Zhang, “Modal Parameter identification of Structure under Base Excitation”,Vol.21, No.4, pp.244-2485, Journal of Mechanical Strength (In China), 1999.
49 Zhu YuanFu, “Vibration Test Simulation for the Complex Structural System.”, Structure & Enviorment Engineering, 2003, Vol. 30, No. 4, pp.59-64.
50 H. Y. Kim, “Vibration-Based Damage Idenentification Using Reconstructured FRFS in Composite Structures”, Journal of Sound and Vibration, Vol. 259, No.5, pp.1131-1146, 2003.
51 T. E. Matikas, “Specimen Design for Fatigue Testing at Very High Frequency”, Journal of Sound and Vibration, Vol. 247, No.4, pp.673-681, 2001.
52 M. Matsuishi and T. Endo, “Fatigue of Metals Subjected to Varying Stress”, paper presented to Japan Society of Mecanical Engineers, Fukuoka, Japan, March 1968.
53 American Society for Testing and Materials,Annual Book of ASTM
Vol,03.01-Metals-Mechanical testing;Elevated and Low-Temperature. Tests, ASTM, Philadelphia, 1986, pp.836-848.
54 楊錦瑤，“固體火箭發動機老化及壽限預估問題探討”，新新季刊，第十六卷，第一期，pp.100-108 ，(1988)。
55 蘇富湖，“藥柱壽限預估”，新新雙月刊，第廿四卷，第四期，pp.97-105 ，(1995)

指導教授

黃俊仁(Jiun-Ren, Hwang)

審核日期

2006-7-18

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