Probabilities of occurrence and detection of damage in airframe materials

被引:49
作者
Harlow, DG [1 ]
Wei, RP [1 ]
机构
[1] Lehigh Univ, Dept Mech Engn & Mech, Bethlehem, PA 18015 USA
关键词
airworthiness; ageing aircraft; corrosion fatigue cracking; pitting corrosion; probability of detection; probability of occurrence;
D O I
10.1046/j.1460-2695.1999.00168.x
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The reliability of airworthiness assessment and the effective management of ageing fleets of aircraft depend critically on the quality of tools for predicting damage nucleation and accumulation and its detection, i.e. on the interrelationship between the probabilities of occurrence and detection. To illustrate these interrelationships, a mechanistically based probability approach involving localized pitting corrosion and subsequent fatigue cracking is presented. A probability of detection based on a typical state-of-the-art technique for non-destructive evaluation is used for comparison and probabilistic assessment. The results suggest that the probability of detection is inadequate, and information on damage size should be included as part of an effective airworthiness assurance methodology hn appropriate target for detecting and sizing damage of approximate to 0.10 mm with a probability of detection and a confidence level of at least 90% is suggested, versus the current capability of 1.27 mm at only 50%.
引用
收藏
页码:427 / 436
页数:10
相关论文
共 14 条
[1]  
BERENS AP, 1989, NONDESTRUCTIVE EVALU, V17, P689
[2]  
BERENS AP, 1991, WLTR913066 USAF, V1
[3]   Transition from pitting to fatigue crack growth - Modeling of corrosion fatigue crack nucleation in a 2024-T3 aluminum alloy [J].
Chen, GS ;
Wan, KC ;
Gao, M ;
Wei, RP ;
Flournoy, TH .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1996, 219 (1-2) :126-132
[4]  
Hagemaier D, 1997, MATER EVAL, V55, P25
[5]   A probability model for the growth of corrosion pits in aluminum alloys induced by constituent particles [J].
Harlow, DG ;
Wei, RP .
ENGINEERING FRACTURE MECHANICS, 1998, 59 (03) :305-325
[6]   PROBABILITY APPROACH FOR PREDICTION OF CORROSION AND CORROSION-FATIGUE LIFE [J].
HARLOW, DG ;
WEI, RP .
AIAA JOURNAL, 1994, 32 (10) :2073-2079
[7]  
HYATT RW, 1991, MATER EVAL, V49, P1402
[8]  
KOMOROWSKI JP, 1998, ICAF97 FATIGUE NEW A, V1, P251
[9]  
LEE B, 1999, THESIS LEHIGH U
[10]   A technique for studying the 3-dimensional shape of corrosion pits [J].
Liao, CM ;
Chen, GS ;
Wei, RP .
SCRIPTA MATERIALIA, 1996, 35 (11) :1341-1346