Probabilistic Vibration Analysis of a Mistuned Integrally Bladed Disk

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Abstract. The objective of this paper is to probabilistically evaluate the effects of mistuned sectors on the dynamic characteristics of an integrally bladed disk (blisk). Small blade to blade physical variation in a disk is termed as mistuning. In this study, the dynamic characteristics of the perfectly tuned blisk were firstly analysed as a baseline. Secondly, a probabilistic approach is used for the mistuning analysis of a blisk. A reduced-order method named as the subset of nominal modes (SNM) was used to generate modes for a mistuned blisk from a cyclic perfectly tuned FE model without creating the full model. Furthermore, as only the modes with natural frequencies close to the modes of interest were considered, a relatively shorter computational time and a much smaller model size than a full blisk model is used. Therefore, the dynamic characteristics of the forced response for random mistuned blisks were obtained.

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Advanced Materials Research (Volumes 891-892)

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726-731

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March 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] J.H. Griffin, and T.M. Hoosac, Model development and statistical investigation of turbine blade mistuning, J. of Vibration, Acoustic, Stress and Reliability in Design, Vol. 106, No. 2, pp.204-210. (1984).

DOI: 10.1115/1.3269170

Google Scholar

[2] M.P. Mignolet, and C.C. Lin, The combined closed-form perturbation approach to the analysis of mistuned bladed disks, J. of Turbomechinery, Vol. 114, pp.771-780. (1993).

DOI: 10.1115/1.2929315

Google Scholar

[3] M.T. Bah, et al, Forced response statistics of mistuned bladed disks: a stochastic reduced basis approach, J. of Sound and Vibration, Vol. 263, pp.377-397. (2003).

DOI: 10.1016/s0022-460x(02)01058-1

Google Scholar

[4] A. Sinhn, Computation of statistics of forced response of mistuned bladed disk assembly via polynormal chaos, J. of Sound and Vibration, Vol 128, pp.449-457. (2006).

DOI: 10.1115/1.2215620

Google Scholar

[5] S.Y. Lee, et al, Assessment of probabilistic methods for mistuned bladed disk vibration, Proceedings of 46th AIAA/ASME/AHS/ASC structures, structural dynamics & materials conference, Austin, USA. (2005).

DOI: 10.2514/6.2005-1990

Google Scholar

[6] M.T. Yang, and J.H. Griffin, A reduced order model of mistuning using a subset of nominal system modes, J. of Engineering for Gas Turbine and Power, Vol. 123, No. 4, pp.893-900. (2001).

DOI: 10.1115/1.1385197

Google Scholar

[7] ANSYS Inc., Mechanical User Guide. Pittsburgh, U.S. (2010).

Google Scholar

[8] The Mathworks Inc., MATLAB 6 Getting Started Guide. Massachusetts, U.S. (2000).

Google Scholar

[9] C. Joseph, etc, Forced response of bladed disk assemblies – a survey, The shock and Vibration Digest, Vol. 31, No. 1. (1999).

DOI: 10.1177/058310249903100102

Google Scholar

[10] G. Chen and J. Hou, Analysis of a mistuning pattern for an integrally bladed disk, the Proceedings of 15th Australian International Aerospace Congress, Australia. (2013).

Google Scholar