FEA on Vibration Characteristics of a Shrouded Turbine Blade

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Abstract:

This paper introduces a FEA method for vibration characteristics analysis of an aero-engine shrouded turbine blade and makes an actual modal analysis of this shrouded blade based on this method in UG software environment. The first six natural frequencies and mode shapes of this shrouded blade are calculated. And also, the dynamic characteristics of the shrouded turbine blade are discussed in detail according to the analysis results. The FEA method and the vibration characteristics analysis results in the paper can be used for optimal design and vibration safety verification of this aero-engine shrouded turbine blade.

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443-447

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July 2012

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] J. Zhang, X.P. Liu, Principle and Numerical Methods of Modal Analysis to Turbo-machines (National Defence Industry Press, China 2001), pp.333-369 (In Chinese).

Google Scholar

[2] W.Q. Zhao, Y.X. Liu, Vibration analysis of aeroengine compressor blade-disc coupling system, Applied mechanics and Materials, Vols. 16-19, pp, 264-268, (2009).

DOI: 10.4028/www.scientific.net/amm.16-19.264

Google Scholar

[3] Shlyanikov V N and Stepanov NV: Engineer Failure Analysis, Vol. 8 (2001) No. 5, pp.461-475.

Google Scholar

[3] Shlyanikov V N and Stepanov NV: Engineer Failure Analysis, Vol. 8 (2001) No. 5, pp.461-475.

Google Scholar

[4] Yang Qingfo, Li Yan, Dynamic analysis and structural modification of Engineer block [C]. In New York Proceedings of the 9th MAC, (1991).

Google Scholar

[5] Wang Z, Three-dimensional Theory and Design Method of Bowed-twisted Blade and its Application to Turbomachines. VKILS, 1999-02(1999).

Google Scholar

[6] D.K. Shen, Strength Calculation of Aero-engine (National Defence Industry Press, China 1990), pp.1-30.

Google Scholar

[7] Chen lulu, Experiment of vibration and response of blade with dry friction structure. Journal of Aerospace Power, 2008, 23(9): 1647-1653.

Google Scholar

[8] Shan Y C, Application and development of platform friction damper for depressing resonant vibration of blades. Journal of Aerospace Power, 16(2): 218-223, (2001).

Google Scholar