Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems
Cable control systems are widely used in aircraft and gliders. This paper deals with the problem of collecting real loads acting cable control systems and cable tests preparation (load spectrum) and performance. The author proposes a method for defining real loads acting on control systems, preparin...
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Format: | Article |
Language: | English |
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Sciendo
2020-12-01
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Series: | Fatigue of Aircraft Structures |
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Online Access: | https://doi.org/10.2478/fas-2020-0010 |
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author | Brzęczek Józef |
author_facet | Brzęczek Józef |
author_sort | Brzęczek Józef |
collection | DOAJ |
description | Cable control systems are widely used in aircraft and gliders. This paper deals with the problem of collecting real loads acting cable control systems and cable tests preparation (load spectrum) and performance. The author proposes a method for defining real loads acting on control systems, preparing and carrying out fatigue tests of cables revealing symptoms of fretting. The fatigue tests results can be used to predict service life, to plan and prepare periodic and details inspections. This method could be used to increase service life of aircraft control cables and could help to replace the commonly used Time-Based Maintenance (TBM) strategy with the Damage Tolerance (DT). |
first_indexed | 2024-04-11T02:19:03Z |
format | Article |
id | doaj.art-19e230dc1e7e4fe9be681ef94cf162ff |
institution | Directory Open Access Journal |
issn | 2300-7591 |
language | English |
last_indexed | 2024-04-11T02:19:03Z |
publishDate | 2020-12-01 |
publisher | Sciendo |
record_format | Article |
series | Fatigue of Aircraft Structures |
spelling | doaj.art-19e230dc1e7e4fe9be681ef94cf162ff2023-01-03T00:21:04ZengSciendoFatigue of Aircraft Structures2300-75912020-12-0120201210211210.2478/fas-2020-0010Some Comments on Fatigue Life Tests of Aircraft Cable Control SystemsBrzęczek Józef0Department of Components Manufacturing and Production Organization, Faculty of Mechanics and Technology, Rzeszow University of Technology, Kwiatkowskiego 4, 37-450 Stalowa Wola, PolandCable control systems are widely used in aircraft and gliders. This paper deals with the problem of collecting real loads acting cable control systems and cable tests preparation (load spectrum) and performance. The author proposes a method for defining real loads acting on control systems, preparing and carrying out fatigue tests of cables revealing symptoms of fretting. The fatigue tests results can be used to predict service life, to plan and prepare periodic and details inspections. This method could be used to increase service life of aircraft control cables and could help to replace the commonly used Time-Based Maintenance (TBM) strategy with the Damage Tolerance (DT).https://doi.org/10.2478/fas-2020-0010aircraft’s cable control systemscable service lifecable fatigue tests |
spellingShingle | Brzęczek Józef Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems Fatigue of Aircraft Structures aircraft’s cable control systems cable service life cable fatigue tests |
title | Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems |
title_full | Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems |
title_fullStr | Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems |
title_full_unstemmed | Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems |
title_short | Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems |
title_sort | some comments on fatigue life tests of aircraft cable control systems |
topic | aircraft’s cable control systems cable service life cable fatigue tests |
url | https://doi.org/10.2478/fas-2020-0010 |
work_keys_str_mv | AT brzeczekjozef somecommentsonfatiguelifetestsofaircraftcablecontrolsystems |