Failure of the tail rotor of the Mi-24 helicopter as a result of a long-term impact of spatial resonance coupling
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Abstract The most important element that has an impact on the safety of flight includes the helicopter power plant and the transmission shaft assembly. Monitoring with the use of the traditional vibroacoustic techniques does not provide satisfactory results. It is especially difficult to detect spatial resonance couplings, which may result in dangerous and rapid breaking of elements. This article focuses on a specific mechanism for formation and deepening of resonance and effects of resonance couplings of two subassemblies. For their monitoring, the FAM-C method was applied. It uses an on-board generator as a sensor. This is a synchronous method, which enables one to detect the onset of spatial resonance.
1993 ◽
Vol 50
(3)
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pp. 627-637
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2009 ◽
Vol 11
(2)
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pp. 425
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2019 ◽
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