Email this article Tribodiagnostics of aviation reduction gears according to the stages of the surface fatigue wear for its units
- Authors: Shabalinskaya L.A.1, Golovanov V.V.1, Bubnova E.S.1, Melnikov A.O.1, Grigorev A.V.2, Prodanov E.S.2
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Affiliations:
- Baranov Central Institute of Aviation Motors
- AO “KLIMOV”
- Issue: Vol 38, No 4 (2017)
- Pages: 297-301
- Section: Article
- URL: https://ogarev-online.ru/1068-3666/article/view/228792
- DOI: https://doi.org/10.3103/S1068366617040122
- ID: 228792
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Abstract
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.
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About the authors
L. A. Shabalinskaya
Baranov Central Institute of Aviation Motors
Author for correspondence.
Email: shabl@ciam.ru
Russian Federation, Moscow, 111116
V. V. Golovanov
Baranov Central Institute of Aviation Motors
Email: shabl@ciam.ru
Russian Federation, Moscow, 111116
E. S. Bubnova
Baranov Central Institute of Aviation Motors
Email: shabl@ciam.ru
Russian Federation, Moscow, 111116
A. O. Melnikov
Baranov Central Institute of Aviation Motors
Email: shabl@ciam.ru
Russian Federation, Moscow, 111116
A. V. Grigorev
AO “KLIMOV”
Email: shabl@ciam.ru
Russian Federation, St. Petersburg, 194100
E. S. Prodanov
AO “KLIMOV”
Email: shabl@ciam.ru
Russian Federation, St. Petersburg, 194100
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