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


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

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

补充文件

附件文件
动作
1. JATS XML

版权所有 © Allerton Press, Inc., 2017