Abstract
The main attention of this article is focused on dynamic loads affecting transmission shafts in the slat and flap transmission systems as well as undesirable effects resulting from these interactions. The article refers to the RTCA aviation standard DO-160G (Environmental Conditions and Test Procedures for Airborne Equipment) regulating the requirements of individual aircraft also from the point of view of vibration in individual zones of the aircraft. The article will focus on two basic load cases: high-level, short duration transient vibration that occurs during an engine fan blade loss and the random vibrations case on an aircraft related to take-off, flight and landing described by the function of power spectral density.
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Ptak, M., Czmochowski, J. (2021). Analysis of the Impact of Dynamic Loads on Transmission Shafts of a Civil Aircraft. In: Mężyk, A., Kciuk, S., Szewczyk, R., Duda, S. (eds) Modelling in Engineering 2020: Applied Mechanics. SMWM 2020. Advances in Intelligent Systems and Computing, vol 1336. Springer, Cham. https://doi.org/10.1007/978-3-030-68455-6_22
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