Nonparametric modeling of random uncertainties for dynamic response of mistuned bladed disks

被引:46
作者
Capiez-Lernout, E [1 ]
Soize, C [1 ]
机构
[1] Univ Marne La Vallee, Mech Engn Lab, F-77454 Marne La Vallee 02, France
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2004年 / 126卷 / 03期
关键词
D O I
10.1115/1.1760527
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The random character of blade mistuning is a motivation to construct probability models of random uncertainties. Recently, a new approach known as a nonparametric model of random uncertainties, based on the entropy optimization principle, was introduced for modeling random uncertainties in linear and nonlinear elastodynamics. This paper presents an extension of this nonparametric model for vibration analysis of structures with cyclic geometry. In particular this probability model allows the blade eigenfrequencies uncertainties and the blade-modal-shape uncertainties to be modeled.
引用
收藏
页码:610 / 618
页数:9
相关论文
共 18 条
[1]   Component-mode-based reduced order modeling techniques for mistuned bladed disks - Part I: Theoretical models [J].
Bladh, R ;
Castanier, MP ;
Pierre, C .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2001, 123 (01) :89-99
[2]   COUPLING OF SUBSTRUCTURES FOR DYNAMIC ANALYSES [J].
CRAIG, RR ;
BAMPTON, MCC .
AIAA JOURNAL, 1968, 6 (07) :1313-&
[3]   EFFECTS OF DETUNING UPON FORCED VIBRATIONS OF BLADED DISKS [J].
EWINS, DJ .
JOURNAL OF SOUND AND VIBRATION, 1969, 9 (01) :65-&
[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]   An adaptive perturbation scheme for the analysis of mistuned bladed disks [J].
Lin, CC ;
Mignolet, MP .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1997, 119 (01) :153-160
[6]   Effects of damping and damping mistuning on the forced vibration response of bladed disks [J].
Lin, CC ;
Mignolet, MP .
JOURNAL OF SOUND AND VIBRATION, 1996, 193 (02) :525-543
[7]   THE COMBINED CLOSED FORM-PERTURBATION APPROACH TO THE ANALYSIS OF MISTUNED BLADED DISKS [J].
MIGNOLET, MP ;
LIN, CC .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1993, 115 (04) :771-780
[8]  
Mignolet MP, 2001, J ENG GAS TURB POWER, V123, P395, DOI 10.1115/1.1338949
[9]  
Ohayon R, 1998, STRUCTURAL ACOUSTICS
[10]   Identification of mistuning characteristics of bladed disks from free response data - Part II [J].
Rivas-Guerra, AJ ;
Mignolet, MP ;
Delor, JP .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2001, 123 (02) :404-411