The Model Of One-Type Aircraft Fleet Behaviour While Service And Advantages SHM V. NDT Implementation

The paper defines the essence of durability characteristics of the designing structure of an airframe in terms of flight safety. Particular attention is drawn to one of the main factors influencing the durability characteristics of the airframe – diagnostics system for the health assessment of the a...

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Main Authors: Lewitowicz Jerzy, Kustroń Kamila
Format: Article
Language:English
Published: Sciendo 2014-12-01
Series:Journal of KONBiN
Subjects:
NDT
SHM
Online Access:http://www.degruyter.com/view/j/jok.2014.30.issue-1/jok-2014-0014/jok-2014-0014.xml?format=INT
id doaj-art-22b3e4c73a0446d098e7b3b5d0720ff2
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spelling doaj-art-22b3e4c73a0446d098e7b3b5d0720ff22018-09-02T18:14:03ZengSciendoJournal of KONBiN2083-46082014-12-01301475810.2478/jok-2014-0014jok-2014-0014The Model Of One-Type Aircraft Fleet Behaviour While Service And Advantages SHM V. NDT ImplementationLewitowicz Jerzy0Kustroń Kamila1Instytut Techniczny Wojsk lotniczych, Wydział Mechaniczny Energetyki i Lotnictwa Politechniki WarszawskiejInstytut Techniczny Wojsk lotniczych, Wydział Mechaniczny Energetyki i Lotnictwa Politechniki WarszawskiejThe paper defines the essence of durability characteristics of the designing structure of an airframe in terms of flight safety. Particular attention is drawn to one of the main factors influencing the durability characteristics of the airframe – diagnostics system for the health assessment of the airframe during the process of operation. The effectiveness of the use of integrated solutions to the structure of the airframe providing a continuous assessment of the technical condition is presented. Continuous diagnostics system integrated with the airframe, SHM, is classified as an intelligent solution. This paper presents a model of the behavior of one-type aircraft operating in the air operator’s fleet in terms of susceptibility to failure. Justified assumption in the description of this behavior, in the form of a “bathtub curve”. The analysis is supported by real data of failures. The benefits of using a continuous diagnostics system integrated with the airframe, SHM, is interpreted in relation to the classical approach with the use of non-destructive testing, NDT, for the three phases of the bathtub curve.http://www.degruyter.com/view/j/jok.2014.30.issue-1/jok-2014-0014/jok-2014-0014.xml?format=INTcivil aviation systemthe air operatorairframedurabilitysmart technology in health assessmentintensity of failuresdiagnosticsNDTSHMpłatowiecintensywność uszkodzeń modelowaintensywność uszkodzeń rzeczywistadiagnostykaNDTSHM
institution Open Data Bank
collection Open Access Journals
building Directory of Open Access Journals
language English
format Article
author Lewitowicz Jerzy
Kustroń Kamila
spellingShingle Lewitowicz Jerzy
Kustroń Kamila
The Model Of One-Type Aircraft Fleet Behaviour While Service And Advantages SHM V. NDT Implementation
Journal of KONBiN
civil aviation system
the air operator
airframe
durability
smart technology in health assessment
intensity of failures
diagnostics
NDT
SHM
płatowiec
intensywność uszkodzeń modelowa
intensywność uszkodzeń rzeczywista
diagnostyka
NDT
SHM
author_facet Lewitowicz Jerzy
Kustroń Kamila
author_sort Lewitowicz Jerzy
title The Model Of One-Type Aircraft Fleet Behaviour While Service And Advantages SHM V. NDT Implementation
title_short The Model Of One-Type Aircraft Fleet Behaviour While Service And Advantages SHM V. NDT Implementation
title_full The Model Of One-Type Aircraft Fleet Behaviour While Service And Advantages SHM V. NDT Implementation
title_fullStr The Model Of One-Type Aircraft Fleet Behaviour While Service And Advantages SHM V. NDT Implementation
title_full_unstemmed The Model Of One-Type Aircraft Fleet Behaviour While Service And Advantages SHM V. NDT Implementation
title_sort model of one-type aircraft fleet behaviour while service and advantages shm v. ndt implementation
publisher Sciendo
series Journal of KONBiN
issn 2083-4608
publishDate 2014-12-01
description The paper defines the essence of durability characteristics of the designing structure of an airframe in terms of flight safety. Particular attention is drawn to one of the main factors influencing the durability characteristics of the airframe – diagnostics system for the health assessment of the airframe during the process of operation. The effectiveness of the use of integrated solutions to the structure of the airframe providing a continuous assessment of the technical condition is presented. Continuous diagnostics system integrated with the airframe, SHM, is classified as an intelligent solution. This paper presents a model of the behavior of one-type aircraft operating in the air operator’s fleet in terms of susceptibility to failure. Justified assumption in the description of this behavior, in the form of a “bathtub curve”. The analysis is supported by real data of failures. The benefits of using a continuous diagnostics system integrated with the airframe, SHM, is interpreted in relation to the classical approach with the use of non-destructive testing, NDT, for the three phases of the bathtub curve.
topic civil aviation system
the air operator
airframe
durability
smart technology in health assessment
intensity of failures
diagnostics
NDT
SHM
płatowiec
intensywność uszkodzeń modelowa
intensywność uszkodzeń rzeczywista
diagnostyka
NDT
SHM
url http://www.degruyter.com/view/j/jok.2014.30.issue-1/jok-2014-0014/jok-2014-0014.xml?format=INT
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