A reduced-order model of mistuning using a subset of nominal system modes

被引:279
作者
Tang, MT [1 ]
Griffin, JH [1 ]
机构
[1] Carnegie Mellon Univ, Dept Mech Engn, Pittsburgh, PA 15213 USA
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2001年 / 123卷 / 04期
关键词
D O I
10.1115/1.1385197
中图分类号
TH [机械、仪表工业];
学科分类号
0802 [机械工程];
摘要
Reduced-order models have been reported in the literature that can be used to predict the harmonic response of mistuned bladed disks. It has been shown that in many cases they exhibit structural fidelity comparable to a finite element analysis of the full bladed disk system while offering a significant improvement in computational efficiency. In these models the blades and disk are treated as distinct substructures. This paper presents a new, simpler approach for developing reduced-order models in which the modes of the mistuned system are represented in terms of a subset of nominal system modes. It has the following attributes: the input requirements are relatively easy to generate; it accurately predicts mistuning effects in regions where frequency veering occurs; as the number of degrees-of-freedom increases it converges to the exact solution; it accurately predicts stresses as well as displacements; and it accurately models the deformation and stresses at the blades' bases.
引用
收藏
页码:893 / 900
页数:8
相关论文
共 13 条
[1]
CRAWLEY EF, 1988, AGARD MANUAL AEROELE, V2
[2]
RESONANT VIBRATION LEVELS OF A MISTUNED BLADED DISK [J].
EWINS, DJ ;
HAN, ZS .
JOURNAL OF VIBRATION ACOUSTICS STRESS AND RELIABILITY IN DESIGN-TRANSACTIONS OF THE ASME, 1984, 106 (02) :211-217
[3]
FABUNMI JA, 1980, ASME, V102, P322
[4]
MODEL DEVELOPMENT AND STATISTICAL INVESTIGATION OF TURBINE BLADE MISTUNING [J].
GRIFFIN, JH ;
HOOSAC, TM .
JOURNAL OF VIBRATION ACOUSTICS STRESS AND RELIABILITY IN DESIGN-TRANSACTIONS OF THE ASME, 1984, 106 (02) :204-210
[5]
A REDUCED-ORDER MODEL OF UNSTEADY FLOWS IN TURBOMACHINERY [J].
HALL, KC ;
FLOREA, R ;
LANZKRON, PJ .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1995, 117 (03) :375-383
[6]
Kruse M.J., 1996, P 37 AIAA ASME STRUC, P1938
[7]
LIN CC, 1997, ASME, V119, P153
[8]
Pidaparti RMV, 1996, J SOUND VIB, V193, P934, DOI 10.1006/jsvi.1996.0324
[9]
A HIGHER-ORDER TECHNIQUE TO COMPUTE THE STATISTICS OF FORCED RESPONSE OF A MISTUNED BLADED DISK ASSEMBLY [J].
SINHA, A ;
CHEN, S .
JOURNAL OF SOUND AND VIBRATION, 1989, 130 (02) :207-221
[10]
WEI ST, 1988, ASME, V110, P429