Asymptotic Description of Maximum Mistuning Amplification of Bladed Disk Forced Response

被引:98
作者
Martel, Carlos [1 ]
Corral, Roque [2 ]
机构
[1] Univ Politecn Madrid, ETSI Aeronauticos, E-28040 Madrid, Spain
[2] Ind Turbopropulsores SA, Madrid 28830, Spain
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2009年 / 131卷 / 02期
关键词
blades; discs (structures); perturbation techniques; springs (mechanical); vibrations; VIBRATION; ASSEMBLIES; MODEL;
D O I
10.1115/1.2968868
中图分类号
TH [机械、仪表工业];
学科分类号
120111 [工业工程];
摘要
The problem of determining the maximum forced response vibration amplification that can be produced just by the addition of a small mistuning to a perfectly cyclical bladed disk still remains not completely clear. In this paper we apply a recently introduced perturbation methodology, the asymptotic mistuning model (AMM), to determine which are the key ingredients of this amplification process and to evaluate the maximum mistuning amplification factor that a given modal family with a particular distribution of tuned frequencies can exhibit. A more accurate upper bound for the maximum forced response amplification of a mistuned bladed disk is obtained from this description, and the results of the AMM are validated numerically using a simple mass-spring model.
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页数:10
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