Diagnostics of gas turbine engine blades using the forced vibration method

被引：0
|
作者：
Kochergin A.V. [1 ]
Ivshin I.V. [1 ]
Sabirov A.R. [1 ]
Gavrilov V.A. [1 ]
机构：
[1] Kazan Higher Artillery Command Engineering School, Kazan
来源：
Russian Aeronautics (Iz VUZ) | 2007年 / 50卷 / 3期
关键词：
RUSSIAN Aeronautic; Compressor Blade; Ampere Force; Diagnostic Complex; Root Attachment;
D O I：
10.3103/S1068799807030178
中图分类号：
学科分类号：
摘要：
The results of experimental studies with the aid of the forced vibration method to determine the technical condition of GTE turbine blades are presented; the phase difference of two vibrations was used as a diagnostic indicator. The schemes of a diagnostic complex are given, the experiment procedure and results obtained are described. © Allerton Press, Inc. 2007.
引用
收藏
页码：330 / 332
页数：2
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