Jan D. Achenbach2013远东论坛大会报告的题目和摘要

2013-3-1 19:17| 发布者: 强天鹏| 查看: 3772| 评论: 0

Probabilistic Considerations for Growth and Detection of Fatigue Cracks and Impact-Generated Delaminations in Aircraft Structures

 

Jan D. Achenbach

McCormick School of Engineering and Applied Science

Northwestern University

Evanston, IL 60208 USA

 

for presentation at

2013 Far East Forum on Nondestructive Evaluation/Testing: New Technology & Applications

June 18-21, 2013,

Jinan, China

 

         Diagnostic techniques provide the input for prognostics. Modeling of constitutive properties, supported by experimental results, provides damage growth laws which in turn provide information on damage evolution and remaining life. Depending on its magnitude, the resulting statement of failure probability may either result in a recommendation for repair or replacement of a structural component, or for an additional cycle in the diagnostics/prognostics loop of the structural health management system.

         In this lecture, I will devote particular attention to the probabilistic aspects of diagnostics and prognostics. Probabilistic considerations play a dominant role in the four stages of the diagnostics and prognostics of fatigue damage in metals. Considerable attention has been given to the evolution and detection of pre-crack fatigue damage and probabilistic aspects of subsequent macrocrack formation (Stage 1). For Stage 2 (macrocrack growth and detection), Paris’s law for crack growth under cyclic loading conditions can be useful, particularly if placed in a probabilistic context. By introducing the probability of detection concept, various probabilities related to the existence, after N cycles, of a crack larger than critical size, some based on a Bayesian approach, can be determined in Stage 3 for the purposes of prognostication. An example is given for fatigue cracks emanating from rivet holes in a lap joint. An analogous probabilistic approach will be presented for the generation of delaminations in laminated fiber-epoxy composites by repeated impact loads.

Significant progress in QNDE has been achieved. On the other hand, SHM has not yet broken through in a big way. SHM systems are often not yet affordably maintainable with near-zero false alarm rates. Huge benefits can, however, be achieved if SHM can justify reduced design margins, longer life spans and reduced service interruptions.

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