Temat: cable systems - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems
Autorzy:: Brzęczek, Józef
Powiązania:: https://bibliotekanauki.pl/articles/2105148.pdf
Data publikacji:: 2020
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:: aircraft’s cable control systems
cable service life
cable fatigue tests
Opis:: 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).
Źródło:: Fatigue of Aircraft Structures; 2020, 12; 102--112
2081-7738
2300-7591
Pojawia się w:: Fatigue of Aircraft Structures
Dostawca treści:: Biblioteka Nauki

Artykuł

Skocz do pozycji: 2.

Tytuł:: The Fatigue Life of Cables in Aircraft Flight Control Systems
Autorzy:: Kubryn, M.
Gruszecki, H.
Pieróg, L.
Chodura, J.
Pietruszka, J.
Brzęczek, J.
Powiązania:: https://bibliotekanauki.pl/articles/98016.pdf
Data publikacji:: 2018
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:: fatigue
cable flight control systems
cable endurance tests
Opis:: The cable flight control systems are commonly used for the control of small airplanes. In these systems, the cables are the only elements transmitting loads from the pilot to the control surfaces. During a flight the cables are moving through pulleys and are subjected to variable loads. A simple analysis of stress in the cable shows that the stress generated by the cyclical bending on the pulleys causes the fatigue of the wires. This phenomenon was noticed on a military aircraft of the M28 family during periodic maintenance inspection in 2007. The endurance tests of KSAN cables of the diameter equal to 3.5 mm and 1.8 mm were performed at the PZL MIELEC. The tests showed the limited fatigue life of the cables due to a progressive increase in the number of broken wires.
Źródło:: Fatigue of Aircraft Structures; 2018, 10; 53-62
2081-7738
2300-7591
Pojawia się w:: Fatigue of Aircraft Structures
Dostawca treści:: Biblioteka Nauki

Artykuł

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