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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Main Author: Brzęczek Józef
Format: Article
Language:English
Published: Sciendo 2020-12-01
Series:Fatigue of Aircraft Structures
Subjects:
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).
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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