Application of high-current pulsed electron beams for modifying the surface of gas-turbine engine blades


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

Experimental data on the influence of irradiation by high-current pulsed electron beams (HCPBs) on the physicochemical state of surface layers and operational properties of the blades of gas-turbine engines made of heat-resistant materials are analyzed. It is shown that the microsecond HCPB is a high-efficient tool for modifying the surface of turbine and compressor blades providing high-speed thermal treatment (quenching), material recrystallization in 20–30-μm-thick surface layers, and surface cleaning and smoothing. These processes determine the increase in the fatigue strength of blades (by 10–30%), heat resistance (by a factor of 2–4), and salt corrosion resistance (up to a factor of 6).

作者简介

V. Shulov

Moscow Aviation Institute (Technical University)

编辑信件的主要联系方式.
Email: shulovva@mail.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

A. Gromov

OAO “MMP im. V.V. Chernysheva”

Email: shulovva@mail.ru
俄罗斯联邦, ul. Vishnevaya 7, Moscow, 125362

D. Teryaev

Moscow Aviation Institute (Technical University)

Email: shulovva@mail.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

V. Engel’ko

Research Institute of Electrophysical Equipment

Email: shulovva@mail.ru
俄罗斯联邦, doroga na Metallostroi 1, Metallostroi, St. Petersburg, 189631

补充文件

附件文件
动作
1. JATS XML

版权所有 © Allerton Press, Inc., 2016