The importance of using information about the discovery of fatigue cracks to eliminate any fatigue failure in a fleet of aircraft of the same type and the human factor influence is studied. Numerical estimation of the influence of this information exchange is obtained. The Monte Carlo method was used for modelling the process of inspecting the aircraft fleet and calculating the probability of fatigue failure as a function of the inspection interval, number of aircraft in the fleet, and intensity of the process of bringing new aircraft into operation. First published online: 24 Dec 201
The effect of a strengthening patch applied at a fatigue critical area during service on the safe li...
Abstract: This work presents a methodology for determining the reliability of fracture control plans...
A methodology has been developed for predicting aircraft safety and reliability incorporating both ...
The scientific article addresses the dependence of aircraft fleet safety on the human factor. The ar...
Development of the inspection programme of fatigue-prone aircraft construction under limitation of a...
Aircraft structures have many components. Maintaining high reliability for these structures generall...
Aircraft structures have many components. Maintaining high reliability for these structures generall...
This study provides new insights in the problem of lumpy aircraft spare parts demands by incorporati...
Abstract. The purpose of this work is to incorporate the fatigue statistical scatter to the determin...
Fatigue is the mechanism of progressive damage which may ultimately limit the economic life of an ai...
Probability of failure (PF) of fatigue-prone aircraft (AC) and failure rate (FR) of airline (AL) for...
A mechanical component can break due to repeated load cycling, even if these loads remain well below...
Abstract. Development of the best economic parameter inspection program of fatigue-prone aircraft un...
PDFTech ReportLTR-FA4H2-9402FuselagesStochastic processesCrackingFatigue (Mechanics)AirframesUnited ...
The effect of a strengthening patch applied at a fatigue critical area during service on the safe li...
The effect of a strengthening patch applied at a fatigue critical area during service on the safe li...
Abstract: This work presents a methodology for determining the reliability of fracture control plans...
A methodology has been developed for predicting aircraft safety and reliability incorporating both ...
The scientific article addresses the dependence of aircraft fleet safety on the human factor. The ar...
Development of the inspection programme of fatigue-prone aircraft construction under limitation of a...
Aircraft structures have many components. Maintaining high reliability for these structures generall...
Aircraft structures have many components. Maintaining high reliability for these structures generall...
This study provides new insights in the problem of lumpy aircraft spare parts demands by incorporati...
Abstract. The purpose of this work is to incorporate the fatigue statistical scatter to the determin...
Fatigue is the mechanism of progressive damage which may ultimately limit the economic life of an ai...
Probability of failure (PF) of fatigue-prone aircraft (AC) and failure rate (FR) of airline (AL) for...
A mechanical component can break due to repeated load cycling, even if these loads remain well below...
Abstract. Development of the best economic parameter inspection program of fatigue-prone aircraft un...
PDFTech ReportLTR-FA4H2-9402FuselagesStochastic processesCrackingFatigue (Mechanics)AirframesUnited ...
The effect of a strengthening patch applied at a fatigue critical area during service on the safe li...
The effect of a strengthening patch applied at a fatigue critical area during service on the safe li...
Abstract: This work presents a methodology for determining the reliability of fracture control plans...
A methodology has been developed for predicting aircraft safety and reliability incorporating both ...