View(s) :
1 (0 ULiège)
Download(s) :
2 (0 ULiège)
p. 108-120
For important fatigue-sensitive structures of aircraft whose breakdowns cause serious accidents, it is required to keep their reliability extremely high. In this paper, we discuss inspection strategies for such important structures against fatigue failure. The focus is on the case when there are fatigue-cracks unexpectedly detected in a fleet of aircraft within a warranty period (prior to the first inspection). The paper examines this case and proposes stochastic models for prediction of fatigue-crack growth to determine appropriate inspections intervals. We also do not assume known parameters of the underlying distributions, and the estimation of that is incorporated into the analysis and decision-making. Numerical example is provided to illustrate the procedure.
Gundars Bērziņš, Konstantin N. Nechval, Nicholas A. Nechval, M. Purgailis and V. F. Strelchonok, « Stochastic Models for Prediction of Fatigue-Crack Growth in Aircraft Structure Components », CASYS, 20 | 2008, 108-120.
Gundars Bērziņš, Konstantin N. Nechval, Nicholas A. Nechval, M. Purgailis and V. F. Strelchonok, « Stochastic Models for Prediction of Fatigue-Crack Growth in Aircraft Structure Components », CASYS [Online], 20 | 2008, Online since 10 October 2024, connection on 27 December 2024. URL : http://popups.uliege.be/3041-539x/index.php?id=2836
Mathematical Statistics Department, University of Latvia, Raina Blvd 19, LV-1050, Riga, Latvia
Applied Mathematics Department, Transport and Telecommunication Institute, Lomonosov Street 1, LV-1019, Riga, Latvia
Mathematical Statistics Department, University of Latvia, Raina Blvd 19, LV-1050, Riga, Latvia
Mathematical Statistics Department, University of Latvia, Raina Blvd 19, LV-1050, Riga, Latvia
Informatics Department, Baltic International Academy, Lomonosov Street 4, LV-1019, Riga, Latvia