Study on the optimal design of mistuned bladed disk (Simultaneous optimization of forced and self-excited vibration and amount of unbalance)
Author:
Affiliation:
1. Department of Mechanical and Systems Engineering, Ryukoku University
2. Mitsubishi Heavy Industries, Ltd.
3. Mitsubishi Power, Ltd.
Publisher
Japan Society of Mechanical Engineers
Link
https://www.jstage.jst.go.jp/article/transjsme/87/898/87_20-00368/_pdf
Reference14 articles.
1. Benini, E. and Toffolo, A., Towards a reduction of compressor blade dynamic loading by means of rotor-stator interaction optimization, Proceedings of ASME Turb Expo 2002, GT2002-30396 (2002), pp.667-674.
2. Cigeroglu, E., An, N. and Menq, C.-H., Wedge damper modeling and forced response prediction of frictionally constrained blades, Proceedings of ASME Turb Expo 2007, GT2007-27963 (2007), pp. 519-528.
3. Feiner, D. M. and Griffin, J. H., A fundamental model of mistuning for a single family of modes, Transactions of the ASME, Journal of Turbomachinery, Vol.124 (2002), pp.150-605.
4. Feiner, D. M. and Griffin, J. H., Mistuning identification of bladed disks using a fundamental mistuning model-part 1: theory, Transactions of the ASME, Journal of Turbomachinery, Vol.124 (2002), pp.597-605.
5. Gallus, H.E., Grollius, H. and Lambertz, J., The influence of blade number ratio and blade row spacing on axial-flow compressor stator blade dynamic load and stage Sound pressure level, ASME Journal of Engineering for Power, Vol. 104, No. 3 (1982), pp.633-158.
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