Mistuning identification of bladed disks using a fundamental mistuning model - part II: Application

被引:114
作者
Feiner, DM [1 ]
Griffin, JH [1 ]
机构
[1] Carnegie Mellon Univ, Dept Mech Engn, Pittsburgh, PA 15213 USA
来源
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 2004年 / 126卷 / 01期
关键词
D O I
10.1115/1.1643914
中图分类号
TH [机械、仪表工业];
学科分类号
0802 [机械工程];
摘要
This paper is the second in a two-part study of identifying mistuning in bladed disks. It presents experimental validation of a new method of mistuning identification based on measurements of the vibratory response of the system as a whole. As a system-based method, this approach is particularly suited to integrally bladed rotors, whose blades cannot be removed for individual measurements. The method is based on a recently developed reduced-order model of mistuning called the fundamental mistuning model (FMM) and is applicable to isolated families of modes. Two versions of FMM system identification are applied to the experimental data: a basic version that requires some prior knowledge of the system's properties, and a somewhat more complex version that determines the mistuning completely from experimental data.
引用
收藏
页码:159 / 165
页数:7
相关论文
共 6 条
[1]
A fundamental model of mistuning for a single family of modes [J].
Feiner, DM ;
Griffin, JH .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2002, 124 (04) :597-605
[2]
FEINER DM, 2004, ASME, V126, P150, DOI DOI 10.1115/1.1643913
[3]
JONES KW, 2002, P 7 NAT TURB ENG HIG
[4]
Judge J., 2002, P INT C STRUCT DYN M
[5]
Petrov EP, 2002, P 7 NAT TURB ENG HIG
[6]
Flutter and resonant vibration characteristics of engine blades [J].
Srinivasan, AV .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1997, 119 (04) :742-775