Study on identification of modal parameters of turbomachinery blade and impeller
Author:
Affiliation:
1. Department of Mechanical and Systems Engineering, Ryukoku University
2. Mitsubishi Heavy Industries, Ltd.
3. Mitsubishi Hitachi Power Systems, Ltd.
Publisher
Japan Society of Mechanical Engineers
Link
https://www.jstage.jst.go.jp/article/transjsme/86/886/86_19-00404/_pdf
Reference13 articles.
1. Akiyama, R., Shiohata, K., Nakajima, M. and Yamashita, J., Development of excitation test method for non-synchronous vibration of rotating turbine blade (Measurement of damping of non-synchronous vibration mode), Transactions of the JSME (in Japanese), Vol. 82, No.838 (2016), DOI:10.1299/transjsme.15-00603.
2. Guillaume, P., Verboven, P., Vanlanduit, S., Van der Auweraer, H. and Peeters, B., A poly-reference implementation of the least-squares complex frequency-domain estimator, Proceedings of IMAC 21, the International Modal Analysis Conference (2003), pp.1-9.
3. Huang, Y., Dimitriadis, G., Kielb, R. E. and Li, J., System eigenvalue identification of mistuned bladed disks using least-squares complex frequency-domain method, Proceedings of ASME Turbo Expo 2017, GT2017-63008 (2017), pp.1-9.
4. Kaneko, Y., Mechanical design of blade for gas turbine, Journal of the Gas Turbine Society of Japan, Vol. 133, No. 1 (2005), pp.4-11 (in Japanese).
5. Kaneko, Y., Iizuka, S. and Ikegami, Y., Development of non-contact measurement method of turbomachinery blade vibration (Improved few-probe method), Transactions of the Japan Society of Mechanical Engineers, Series C, Vol. 67, No. 658 (2001), pp.1846-1852 (in Japanese).
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1. Proposition of a single-degree-of-freedom experimental modal analysis method considering the effect of mode components close to the target mode;Transactions of the JSME (in Japanese);2020
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