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The Fatigue Life of Cables in Aircraft Flight Control Systems Cover

The Fatigue Life of Cables in Aircraft Flight Control Systems

Fatigue of Aircraft Structures
Volume 2018 (2018): Issue 10 (December 2018)
By: Mariusz Kubryn,  Henryk Gruszecki,  Leszek Pieróg,  Jerzy Chodur,  Janusz Pietruszka and  Józef Brzęczek  
Open Access
|Jun 2019

References

  1. [1] Russian standard TU 14-4-1266-83 Aviation steel wire ropes “KSAN”.
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  2. [2] Unpublished reports of PZL Mielec.
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  3. [3] Instructions for Use of Pacific T5 Cable Tensiometer. WI-CU-001 T5 Instructions. Opti Manufacturing Corporation.
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  4. [4] Report Accident on 9 August 2007 off the coast of Moorea (French Polynesia) to the DHC6-300 registered F-OIQI operated by Air Moorea. Bureau d’Enquêtes et d’Analyses pour la sécurité de l’aviation civile.
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DOI: https://doi.org/10.2478/fas-2018-0005 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 53 - 62
Published on: Jun 28, 2019
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
fatigue,
cable flight control systems,
cable endurance tests
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2019 Mariusz Kubryn, Henryk Gruszecki, Leszek Pieróg, Jerzy Chodur, Janusz Pietruszka, Józef Brzęczek, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

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