Fatigue of Aircraft Structures (Dec 2020)

Modular Test Stand for Fatigue Testing of Aeronautical Structures – Verification of Assumptions

  • Leski Andrzej,
  • Wronicz Wojciech,
  • Kowalczyk Piotr,
  • Szmidt Michał,
  • Klewicki Robert,
  • Włodarczyk Karol,
  • Uliński Grzegorz

DOI
https://doi.org/10.2478/fas-2020-0008
Journal volume & issue
Vol. 2020, no. 12
pp. 78 – 91

Abstract

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The Modular Test Stand was developed and manufactured to decrease the cost of fatigue testing and reduce the time of its completion as well as to enable testing specimens under more complex load conditions. The stand consists of three connected sections, similar to a wing box, all being loaded in the same way. Thanks to that, several specimens can be tested simultaneously. This configuration requires that stress and strain distribution should be reasonably uniform, as assumed in the design stage. The structure can be loaded with bending or torsion. A whole section, selected structural node or a specimen mounted in the structure as well as a repair or a sensor can be a test object.

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