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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| Authors: | G V Tsybanev M A Ageev R V Titarenko |
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| Affiliation: | (1) Pisarenko Institute of Problems of Strength, National Academy of Sciences of Ukraine, Kiev, Ukraine;(2) “Industrial Association Makarov Yuzhnyi Engineering Plant” State Enterprise, Dnepropetrovsk, Ukraine;(3) Antonov Aviation Scientific and Engineering Complex, Kiev, Ukraine |
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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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Translated from Problemy Prochnosti, No. 4, pp. 87–93, July–August, 2008. |
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| Keywords: | landing gear lever computational scheme stressed state limiting state of the material |
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