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


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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.

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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