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Fatigue of Aircraft Structures

The Journal of Institute of Aviation

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Online
ISSN
2300-7591
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Full Scale Fatigue Test of New Undercarriage for Commuter Aircraft

Józef Brzęczek / Henryk Gruszecki / Leszek Pieróg / Janusz Pietruszka
Published Online: 2013-04-30 | DOI: https://doi.org/10.2478/v10164-012-0058-1

Abstract

Fatigue testing of the new main landing gear for the PZL M28 aircraft was conducted in Polskie Zakłady Lotnicze Sp. z o.o. in Mielec using MTS Aero 90-LT system. The test was conducted in a flight-by-flight manner with loads resulting from landing, taxiing, maneuvering and braking. The undercarriage structure is made of high tensile strength low alloy steel. FEM analyses were performed before the tests in order to find critical points and to obtain information about loads which may be neglected. During the test fatigue damage was observed, which led to splitting the test into two separate tests performed in independent rigs: the test of the undercarriage leg and the test of the shock absorber.

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  • Ref. no. PRG/O/W/64/04. Polskie Zakłady Lotnicze Sp. z o.o., Mielec, May 2007 (in Polish).Google Scholar

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  • Ref. no. PRG/O/W/14/10. Polskie Zakłady Lotnicze Sp. z o.o., Mielec, July 2010 (in Polish).Google Scholar

About the article

Published Online: 2013-04-30

Published in Print: 2012-12-01


Citation Information: Fatigue of Aircraft Structures, ISSN (Online) 2300-7591, DOI: https://doi.org/10.2478/v10164-012-0058-1.

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