Tribodiagnostics of aviation reduction gears according to the stages of the surface fatigue wear for its units

L. A. Shabalinskaya; V. V. Golovanov; E. S. Bubnova; A. O. Melnikov; A. V. Grigorev; E. S. Prodanov

doi:10.3103/S1068366617040122

Tribodiagnostics of aviation reduction gears according to the stages of the surface fatigue wear for its units

Авторы: Shabalinskaya L.A.¹, Golovanov V.V.¹, Bubnova E.S.¹, Melnikov A.O.¹, Grigorev A.V.², Prodanov E.S.²
Учреждения:
1. Baranov Central Institute of Aviation Motors
2. AO “KLIMOV”
Выпуск: Том 38, № 4 (2017)
Страницы: 297-301
Раздел: Article
URL: https://ogarev-online.ru/1068-3666/article/view/228792
DOI: https://doi.org/10.3103/S1068366617040122
ID: 228792

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One method for the early examination of the aviation reduction gear’s state is to predict the rates of process of surface fatigue wear according to the type of fatigue wear particles, which appear in friction units. We perform this investigation based on example of the main reduction gear of the helicopter and reduction gears of the KSA type of MIG-29K/KUB aircraft during their bench testing.