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Analysis of the specific features of loading of the elements of landing gears of aircrafts aimed at the evaluation of the load-bearing capacity of the structure

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Abstract

We propose a computational scheme of the aircraft nose landing gear and perform the analysis of weak sections in the landing-gear lever by the finite-element method. We determine the loading modes in which the landing-gear lever is subjected to disproportional cyclic loads, which should be taken into account in the evaluation of the service life and determination of the properties of applied materials.

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Authors and Affiliations

  1. Pisarenko Institute of Problems of Strength, National Academy of Sciences of Ukraine, Kiev, Ukraine

    G. V. Tsybanev

  2. “Industrial Association Makarov Yuzhnyi Engineering Plant” State Enterprise, Dnepropetrovsk, Ukraine

    M. A. Ageev

  3. Antonov Aviation Scientific and Engineering Complex, Kiev, Ukraine

    R. V. Titarenko

Authors
  1. G. V. Tsybanev
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  2. M. A. Ageev
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  3. R. V. Titarenko
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Translated from Problemy Prochnosti, No. 4, pp. 87–93, July–August, 2008.

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Tsybanev, G.V., Ageev, M.A. & Titarenko, R.V. Analysis of the specific features of loading of the elements of landing gears of aircrafts aimed at the evaluation of the load-bearing capacity of the structure. Strength Mater 40, 458–462 (2008). https://doi.org/10.1007/s11223-008-9056-5

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  • DOI: https://doi.org/10.1007/s11223-008-9056-5

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