Tribodiagnostics of aviation reduction gears according to the stages of the surface fatigue wear for its units
- 作者: 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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隶属关系:
- Baranov Central Institute of Aviation Motors
- AO “KLIMOV”
- 期: 卷 38, 编号 4 (2017)
- 页面: 297-301
- 栏目: Article
- URL: https://journals.rcsi.science/1068-3666/article/view/228792
- DOI: https://doi.org/10.3103/S1068366617040122
- ID: 228792
如何引用文章
详细
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.
作者简介
L. Shabalinskaya
Baranov Central Institute of Aviation Motors
编辑信件的主要联系方式.
Email: shabl@ciam.ru
俄罗斯联邦, Moscow, 111116
V. Golovanov
Baranov Central Institute of Aviation Motors
Email: shabl@ciam.ru
俄罗斯联邦, Moscow, 111116
E. Bubnova
Baranov Central Institute of Aviation Motors
Email: shabl@ciam.ru
俄罗斯联邦, Moscow, 111116
A. Melnikov
Baranov Central Institute of Aviation Motors
Email: shabl@ciam.ru
俄罗斯联邦, Moscow, 111116
A. Grigorev
AO “KLIMOV”
Email: shabl@ciam.ru
俄罗斯联邦, St. Petersburg, 194100
E. Prodanov
AO “KLIMOV”
Email: shabl@ciam.ru
俄罗斯联邦, St. Petersburg, 194100
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