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Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems Cover

Some Comments on Fatigue Life Tests of Aircraft Cable Control Systems

Open Access
|Jul 2021

References

  1. [1] Brzęczek, J. (2019). Examination of Aircraft’s cable Control Systems Tension. Advances in Science and Technology Research Journal, 13(2), 65-71.10.12913/22998624/106238
  2. [2] Certification specifications for CS-23 Normal, Performance, Aerobatic and Local Transport Aircraft, November 14, 2003 and related AMC and FTG.
  3. [3] Hankus, Ł. (2014). Longitudinal strains of hoisting ropes under conditions of complex cyclically changeable loads. (In Polish: Wzdłużne odkształcenia lin wyciągowych w warunkach złożonych obciążeń cyklicznie zmiennych). Przegląd Górniczy, No. 5, 101.
  4. [4] Rzeszow University of Technology. Flight tests of the MP-02 Czajka aircraft – Rzeszów 2019 ‒ unpublished.
  5. [5] Krzysiak, A. (1983). Experimental studies of the hinge torque in terms of sub and sonic speeds. (In Polish: Eksperymentalne badania momentu zawiasowego w zakresie pod i przydźwiękowych prędkości), Transactions of the Institute of Aviation, No. 94, 3-20.
  6. [6] Kubryn, M., Gruszecki, H., Pieróg, L., Chodur, J., Pietruszka, J. and Brzęczek, J. (2018). Fatigue life of cables in aircraft flight control systems. Fatigue of Aircraft Structures, 2018(10), 53-62.10.2478/fas-2018-0005
DOI: https://doi.org/10.2478/fas-2020-0010 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 102 - 112
Published on: Jul 23, 2021
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2021 Józef Brzęczek, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.