介绍了飞机日历寿命研究的技术背景和国内外同类研究概况以及存在的问题.重点对腐蚀环境下飞机结构加速腐蚀试验技术、防腐涂层腐蚀损伤评定技术、腐蚀当量关系和日历寿命理论分析方法等几个关键问题及其技术途径进行了阐述和探讨.
参考文献
| [1] | Simpson, D.L., -;Brooks, CL .Tailoring the structural integrity process to meet the challenges of aging aircraft[J].International Journal of Fatigue,1999(Supplement 1):0-0. |
| [2] | D. G. Harlow;R. P. Wei .A probability model for the growth of corrosion pits in aluminum alloys induced by constituent particles[J].Engineering Fracture Mechanics,1998(3):305-325. |
| [3] | J. Leifer;J. I. Mickalonis .Prediction of aluminum pitting in natural waters via artificial neural network analysis[J].Corrosion: The Journal of Science and Engineering,2000(6):563-571. |
| [4] | H. P. Hong .Application of the stochastic process to pitting corrosion[J].Corrosion: The Journal of Science and Engineering,1999(1):10-16. |
| [5] | Engelhardt G;Strehblow H H .The determination of the shape of developing corrosion pits[J].Corrosion Science,1994,36(10):1711-1725. |
| [6] | Pantelakis SG.;Apostolopoulos CA.;Daglaras PG. .Tensile and energy density properties of 2024, 6013, 8090 and 2091 aircraft aluminum alloy after corrosion exposure[J].Theoretical and Applied Fracture Mechanics,2000(2):117-134. |
| [7] | Evan J;Dolley J .Chemically short-crack behavior of the 7075-T6 aluminum alloy[D].Pennsylvania,Lehigh University,1999. |
| [8] | K. K. Sankaran;R. Perez;K. V. Jata .Effects of pitting corrosion on the fatigue behavior of aluminum alloy 7075-T6: modeling and experimental studies[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2001(1/2):223-229. |
| [9] | D.L. DuQuesnay;P.R. Underhill;H.J. Britt .Fatigue crack growth from corrosion damage in 7075-T6511 aluminium alloy under aircraft loading[J].International Journal of Fatigue,2003(5):371-377. |
| [10] | D.J. Groner;D.E. Nieser .U.S. Air Force Aging Aircraft Corrosion[J].Canadian Aeronautics and Space Journal,1996(2):63-67. |
| [11] | Wei P P;Harlow D G.Corrosion and corrosion fatigue of aluminum alloys-an aging aircraft issue[A].北京:高等教育出版社,1999:2197-2204. |
| [12] | Liao M;Renaud G;Bellinger N C.Effects of exfoliation corrosion on static and fatigue behavior of aircraft materials and structures-testing and modeling studies[A].USA(CA):Palm Springs,2005 |
| [13] | Min Liao;N. C. Bellinger;J. P. Komorowski .Modeling the effects of prior exfoliation corrosion on fatigue life of aircraft wing skins[J].International Journal of Fatigue,2003(9/11):1059-1067. |
| [14] | Liao M;Renaud G;Backman D.Modeling of prior exfoliation corrosion in aircraft wing skins[A].Banff.Alta,Canada,2004 |
| [15] | M. Liao;G. Renaud;N.C. Bellinger .Fatigue modeling for aircraft structures containing natural exfoliation corrosion[J].International Journal of Fatigue,2007(4):677-686. |
| [16] | Sharp P K;Mills T;Russo S.Effects of exfoliation corrosion on the fatigue life of two high-strength aluminum alloys[A].St.Louis,Missouri,USA,2000 |
| [17] | Mills T;Honeycutt K;Brooks C L.Demonstration of an holistic structural integrity process using corrosion/fatigue interactions from laboratory experiments and field experience[A].Solomons,MD,USA,2004 |
| [18] | D.L. DuQuesnay;P.R. Underhill;H.J. Britt .Fatigue crack growth from corrosion damage in 7075-T6511 aluminium alloy under aircraft loading[J].International Journal of Fatigue,2003(5):371-377. |
| [19] | Kumar B;Widener C;Jahn A.Review of the Applicability of FSW Processing to Aircraft Applications[AIAA Paper 2005-2000][A].Austin Texas,USA,2005:1-18. |
| [20] | Panasyuk Y Y;Ratych L V .The methodology of estimating inhibitor effectiveness in corrosion fatigue crack propagation[J].Corrosion Science,1995,37(03):391-412. |
| [21] | Sivaprasada S;Tarafdera S;Ranganathb V R .Corrosion fatigue crack growth behaviour of naval steels[J].Corrosion Science,2006,48(08):1996-2003. |
| [22] | Ruschau J J .Complete fatigue crack growth rate curves for aluminum alloy 2124-T851 including typical crack growth models[Report No.AD-Ao81653,AFML-TR-78-155][R].,1978. |
| [23] | P.V. Petroyiannis;Al.Th. Kermanidis;R. Akid .Analysis of the effects of exfoliation corrosion on the fatigue behaviour of the 2024-T351 aluminium alloy using the fatigue damage map[J].International Journal of Fatigue,2005(7):817-827. |
| [24] | Daniel Kujawski .A new (ΔK+K_max)~0.5 driving force parameter for crack growth in aluminum alloys[J].International Journal of Fatigue,2001(8):733-740. |
| [25] | K. Sadananda;A. K. Vasudevan .Crack tip driving forces and crack growth representation under fatigue[J].International Journal of Fatigue,2004(1):39-47. |
| [26] | liaw P K;Logsdon W A .Fatigue crack growth behavior in In-conel 706 at 297 K and 4.2 K[J].Acta Metallurgica,1988,36(07):1731-1744. |
| [27] | King J E .Surface damage and near-threshold fatigue crack growth in a Ni-base superalloy in vacuum[J].Fatigue & Fracture of Engineering Materials & Structures,1982,5(02):177-188. |
| [28] | Xiulin Zheng;Rong Wang .Overload effects on corrosion fatigue crack initiation life and life prediction of aluminum notched elements under variable amplitude loading[J].Engineering Fracture Mechanics,1999(5):557-572. |
| [29] | R. SUNDER;W. J. PORTER;N. E. ASHBAUGH .The role of air in fatigue load interaction[J].Fatigue & Fracture of Engineering Materials and Structures,2003(1):1-16. |
| [30] | 陈跃良,段成美,吕国志.军用飞机日历寿命预测技术研究现状及关键技术问题[J].中国工程科学,2002(04):69-74. |
| [31] | 张福泽.飞机日历寿命确定的区域定寿法[J].航空学报,2001(06):549-552. |
| [32] | 杨晓华,姚卫星,陈跃良.考虑日历环境影响的结构日历寿命研究[J].应用力学学报,2002(03):157-159. |
| [33] | 杨晓华,姚卫星,段成美.腐蚀环境下LC4铝合金疲劳损伤累积规律研究[J].航空学报,2003(03):234-236. |
| [34] | 周希沅.飞机结构的当量环境谱与加速试验谱[J].航空学报,1996(05):613. |
| [35] | 董登科,王俊扬.关于军用飞机服役日历年限评定用的当量环境谱[J].航空学报,1998(04):0. |
| [36] | 陈群志,李喜明,周希沅,王英利,吴臻,刘文珽,徐晓飞.飞机结构典型环境腐蚀当量关系研究[J].航空学报,1998(04):0. |
| [37] | 蒋冬滨.飞机结构关键危险部位加速腐蚀试验环境谱研究[J].航空学报,1998(04):0. |
| [38] | 陈跃良,段成美,金平,杨晓华.飞机结构局部环境加速腐蚀当量谱[J].南京航空航天大学学报,1999(03):338-341. |
| [39] | 陈跃良,杨晓华,吕国志.结构腐蚀损伤定量预测方法对比研究[J].中国腐蚀与防护学报,2003(01):52-55. |
| [40] | 张福泽.飞机日历寿命确定的新方法研究[M].北京:气象出版社,2000 |
| [41] | 金属机件腐蚀损伤日历寿命的计算模型和确定方法[J].航空学报,1999(01):75. |
| [42] | 张栋.飞机结构件在当量环境谱下加速腐蚀试验和日历寿命估算方法[J].航空学报,2000(03):196-201. |
| [43] | 董登科;王俊扬;薛景川.考虑环境腐蚀试验和日历使用寿命修正方法[J].结构强度研究,1999(02):45-50. |
| [44] | 叶彬.飞机结构腐蚀疲劳寿命预估工程方法研究[J].洪都科技,2003(02):1-6. |
| [45] | 杨玉恭,薛景川,焦坤芳,弓云昭.飞机结构腐蚀疲劳分析中的DFR法[J].机械强度,2004(z1):52-54. |
| [46] | 王斌团,杨庆雄.LC4CS铝合金和30CrMnSiNi2A钢在大气环境预腐蚀后的疲劳曲线[J].机械强度,2000(03):222-223,227. |
| [47] | LY12CZ和7075T7351铝合金在EXCO溶液中腐蚀动力学的统计研究[J].航空学报,1999(01):34. |
| [48] | 航空铝合金大气腐蚀加速试验研究[J].中国腐蚀与防护学报,2005(05):262-266. |
| [49] | 王斌团;范建华;杨庆雄 .金属材料大气环境静态腐蚀老化的疲劳性能[J].金属学报,1999,35(11):1163-1166. |
| [50] | 胡艳玲,李荻,郭宝兰.LY12CZ铝合金型材的腐蚀动力学统计规律研究及日历寿命预测方法探讨[J].航空学报,2000(Z1):53-57. |
| [51] | 刘文珽;李玉海.飞机结构日历寿命体系评定技术[M].北京:航空工业出版社,2004 |
| [52] | Robert C E.Structural health monitoring of composite plates un-der ambient and cryogenic conditions[A].Structural Dynamics & Materials Center,Austin,Texas,USA,2005:18-21. |
| [53] | 刘文卿.实验设计[M].北京:清华大学出版社,2005 |
| [54] | 王岩;隋思涟;王爱青.数理统计与MATLAB工程数据分析[M].北京:清华大学出版社,2006 |
| [55] | 郁大照,陈跃良,段成美.基于神经网络的飞机结构腐蚀损伤统计研究[J].中国腐蚀与防护学报,2006(01):19-21. |
| [56] | 陈群志 .腐蚀环境下飞机结构日历寿命技术体系研究[D].北京航空航天大学,1999. |
| [57] | 陈群志,孙祚东,陆维忠,韩恩厚,常铁军,李京.SEBF/SLF重腐蚀防护涂层应用于典型飞机结构中防腐性能综合评定[J].中国腐蚀与防护学报,2005(06):365-368. |
| [58] | 常红,韩恩厚,王俭秋,柯伟.飞机蒙皮涂层对LY12CZ铝合金腐蚀疲劳寿命的影响[J].中国腐蚀与防护学报,2006(01):34-36,42. |
| [59] | 陈群志;徐晓飞 .JL×飞机典型结构腐蚀环境下服役日历年限与使用寿命评定技术研究(总结报告)[R].中航总公司第623研究所、320厂,1998. |
| [60] | 何宇廷.飞机结构寿命包线的建立[J].空军工程大学学报（自然科学版）,2005(06):4-6. |
| [61] | 何宇廷.基于飞机结构寿命包线的飞机结构单机寿命监控[J].中国工程科学,2006(06):23-27. |
| [62] | He Y T;Fan C H;Zhang H X.Fatigue life supervision of aircraft structures under corrosive conditions[J].Key Engineering Materials,2006(09) |
| [63] | 何宇廷,范超华.飞机结构寿命包线的确定方法[J].空军工程大学学报（自然科学版）,2006(06):1-3. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分：
-
10%
-
20%
-
30%
-
40%
-
50%