The main causes of fractures of the aircraft structures made of steel, aluminum alloys, and titanium alloys are analyzed. On the basis of the experience of operation of “AN” aircrafts, we analyze the methods aimed at the prevention of fractures of metal parts and units of the aircraft equipment.
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V. V. Panasyuk (editor), Fracture Mechanics and Strength of Materials [in Ukrainian], Vol. 9: O. P. Ostash, V. M. Fedirko, V. M. Uchanin, et al., Strength and Durability of Aircraft Materials and Structural Elements [in Ukrainian], Spolom, Lviv (2007).
E. V. Abolikhina and A. G. Molyar, “Corrosion of aircraft structures made of aluminum alloys,” Fiz.-Khim. Mekh. Mater., 39, No. 6, 106–110 (2003); English translation: Mater. Sci., 39, No. 6, 889–894 (2003).
V. A. Trofimov and A. G. Molyar, ‘Specific features of in-service failures of parts of the landing gear of An-124 “Ruslan” aircrafts,” Fiz.-Khim. Mekh. Mater., 37, No. 2, 170–174 (2001); English translation: Mater. Sci., 37, No. 2, 333–339 (2001).
V. A. Trofimov and A. G. Molyar, “Some causes of fracture of load-bearing elements of landing gears made of high-strength steels in Antonov airplanes,” Fiz.-Khim. Mekh. Mater., 38, No. 3, 107–109 (2002); English translation: Mater. Sci., 38, No. 3, 445–448 (2002).
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Translated from Fizyko-Khimichna Mekhanika Materialiv, Vol. 52, No. 1, pp. 14–20, January–February, 2016.
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Bychkov, A.S., Fedirko, V.N. Analysis of the in-Service Failures of Metal Structures of the Aircraft Equipment. Mater Sci 52, 9–16 (2016). https://doi.org/10.1007/s11003-016-9920-6
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DOI: https://doi.org/10.1007/s11003-016-9920-6