期刊文献+

危险蚀坑评判及疲劳寿命计算 被引量:7

JUDGMENT OF CRITICAL PITS AND CALCULATION OF FATIGUE LIFE
下载PDF
导出
摘要 通过对在EXCO(exfoliation corrosion)溶液中加速腐蚀不同时间后的LC4CS试件表面腐蚀形貌进行观测,得到不同腐蚀时间下试件表面蚀坑深度及底部曲率半径。通过分析给出张开角的定义,并以此确定危险蚀坑及预测预腐蚀件的疲劳寿命。研究结果表明:张开角可以合理地确定危险蚀坑以及初始裂纹的等效尺寸。通过算例分析,用张开角来确定危险蚀坑可以较好地预测预腐蚀件的疲劳寿命。 The corrosion morphology of specimens of aluminum alloy LC4CS soaked in EXCO (exfoliation corrosion) solution were examined by microscope to obtain depth of pits and radius of curvature at the bottom of pits with different pre-corrosion times. The definition of opening angle was proposed by analyzing experimental results, so the critical pits was determined and the pre-corrosion fatigue life was predicted based on the opening angle. Calculated life for example showed that opening angle could determine the critical pits and the equivalent dimension of initial crack. Examined by calculating an example, the critical pits determined by opening angle could be used to predict the pre-corrosion fatigue life reasonably.
作者 张川 姚卫星
出处 《机械强度》 CAS CSCD 北大核心 2013年第2期207-213,共7页 Journal of Mechanical Strength
关键词 预腐蚀 张开角 危险蚀坑 疲劳寿命 Pre-corrosion Opening angle Critical pit Fatigue life
  • 相关文献

参考文献18

  • 1Ishihara S, Nan Z Y, McEvily A J, Goshima T, Sunada S. On the initiation and growth behavior of corrosion pits during corrosion fatigue process of industrial pure aluminum [ J ]. International Journal of Fatigue, 2008, 30 : 1659-1668.
  • 2陈定海,郭兵,朱做涛.飞机结构腐蚀损伤尺寸的关联性分析与探讨[J].海军航空工程学院学报,2008,23(2):221-223. 被引量:3
  • 3Medved J J, Breton M, Irving P E. Corrosion pit size distributions and fatigue lives-a study of the EIFS technique for fatigue design in the presence of corrosion [ J ]. International Journal of Fatigue, 2004, 26: 71-80.
  • 4Chaussumier M, Shahzad M, Mabvu C, Chieragatti R, Rezai-Aria F. A fatigue multi-site cracks model using coalescence, short and long crack growth laws, for anodized aluminum alloys [ J ]. Procedia Engineering, 2010, 2: 995-1004.
  • 5Dolley E J, Lee B, Wei R P. The effect of pitting corrosion on fatigue life [ J]. Fatigue Fract Engng Mater Struct, 2000, 23 : 555- 560.
  • 6Yibing Xiang, Yongming Liu. EIFS-based crack growth fatigue life prediction of pitting-corroded test specimens [ J ]. Engineering Fracture Mechanics, 2010, 77: 1314-1324.
  • 7Rokhlin S I, Kim J-Y. In situ ultrasonic monitoring of surface fatigue crack initiation and growth from surface cavity [ J ]. International Journal of Fatigue, 2003, 25:41-49.
  • 8Turnbull A, Wright L, Crocker L. New insight into the pit-to-crack transition from finite element analysis of the stress and strain distribution around a eorrosioin pit [ J]. Corrosion Science, 2010, 52 : 1492-1498.
  • 9Cerit M, Genel K, Eksi S. Numerical investigation on stress concentration of corrosion pit [ J]. Engineering Failure Analysis, 2009, 16: 2467-2472.
  • 10Schmidt C G, Kanazawa C H, Shockley D A, Flournoy T H. Corrosion-fatigue crack nucleation in the ALCLAD layer of 2024T3 commercial aircraft skin [ C ]//Structural Integrity in Aging Aircraft. San Francisco, California : ASME International Mechanical Engineering Congress and Exposition, 1995: 171-174.

二级参考文献20

  • 1穆志韬,柳文林,于战樵.飞机服役环境当量加速腐蚀折算方法研究[J].海军航空工程学院学报,2007,22(3):301-304. 被引量:32
  • 2陈跃良,杨晓华.LY12CZ铝合金力学性能随日历腐蚀环境变化的研究[J].海军航空工程学院学报,2002,17(4):477-479. 被引量:10
  • 3郑立春,姚卫星.疲劳裂纹形成寿命预测方法综述[J].力学与实践,1996,18(4):9-14. 被引量:14
  • 4高镇同.航空金属材料疲劳性能手册[M].北京:北京航空材料研究所,1981..
  • 5Coffin L F. A Study of the Effects of Cyclic Thermal Stresses on a Ductile Metal[J]. Transactions of the American Society of Mechanical Engineers (ASME), 1954, 76: 931-950.
  • 6Manson S S. Behaviour of Materials Under Condition of Thermal Stress [R]. NACA TA- 2933, 1954.
  • 7Jaske C E, Feddersen C E, Davis K B, et al. Analysis of Fatigue, Fatigue Crack Propagation, and Fracture Data[R]. NASA CR--132332, 1973.
  • 8吴学仁.飞机结构金属材料力学性能手册(第一卷)静强度·疲劳/耐久性[M].北京:航空工业出版社,1996.
  • 9Donaldson S L, Kim R Y. Life Prediction of Glass/ Vinylester and Glass/Polyester Composites under Fatigue Loading[C]//Proceedings of the 10th International Conference on Composite Materialsfatigue and Fracture. Cambridge: Woodhead Publishing Limited, 1995 : 557-584.
  • 10Hwang W B, Han K S. Fatigue of Composite Materials Damage Model and Life Prediction[C]// Composite Materials Fatigue and Fracture, Philadelphia:American Society for Testing and Materials(ASTM STP 1012), 1989:87-102.

共引文献19

同被引文献32

引证文献7

二级引证文献21

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部