Tribodiagnostics of aviation reduction gears according to the stages of the surface fatigue wear for its units
- Autores: 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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Afiliações:
- Baranov Central Institute of Aviation Motors
- AO “KLIMOV”
- Edição: Volume 38, Nº 4 (2017)
- Páginas: 297-301
- Seção: Article
- URL: https://journals.rcsi.science/1068-3666/article/view/228792
- DOI: https://doi.org/10.3103/S1068366617040122
- ID: 228792
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Resumo
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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Sobre autores
L. Shabalinskaya
Baranov Central Institute of Aviation Motors
Autor responsável pela correspondência
Email: shabl@ciam.ru
Rússia, Moscow, 111116
V. Golovanov
Baranov Central Institute of Aviation Motors
Email: shabl@ciam.ru
Rússia, Moscow, 111116
E. Bubnova
Baranov Central Institute of Aviation Motors
Email: shabl@ciam.ru
Rússia, Moscow, 111116
A. Melnikov
Baranov Central Institute of Aviation Motors
Email: shabl@ciam.ru
Rússia, Moscow, 111116
A. Grigorev
AO “KLIMOV”
Email: shabl@ciam.ru
Rússia, St. Petersburg, 194100
E. Prodanov
AO “KLIMOV”
Email: shabl@ciam.ru
Rússia, St. Petersburg, 194100
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