Fatigue Damage Prevention on Turbine Blades: Study of Underplatform Damper Shape

Author:

Berruti Teresa1,Firrone Christian M.1,Pizzolante M.1,Gola Muzio M.1ORCID

Affiliation:

1. Politecnico di Torino

Abstract

Forced vibrations can lead to an irreparable damage of a blade array. Devices called “underplatform damper” that dissipate the vibration energy are employed in order to reduce blade vibration amplitude. The present paper deals with the design of the underplatform damper. A numerical code to calculate the forced response of a blade array with dampers has been previously purposely developed. A method is here proposed for the estimation of the unknown contact parameters demanded by the code. The computation results are here validated by means of comparison with experimental results on a static test rig. Three dampers with different shape are tested.

Publisher

Trans Tech Publications, Ltd.

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference5 articles.

1. K.Y. Sanliturk, D.J. Ewins., A.B. Stanbridge: Proceedings of ASME Gas Turbine & Aeroengine Congress and Exhibition, Indianapolis , 1999, ASME paper 99-GT-335.

2. L. Panning, K. Popp, W. Sextro, F. Goetting: Proceedings of ASME GT2004, Vienna, 2004, ASME paper GT2004-53316, p.1.

3. C.M. Firrone, D. Botto, M.M. Gola: Proceedings of ASME ESDA2006, ASME paper ESDA2006-95605, Torino, 2006, p.1.

4. C. Siewert, L. Panning, A. Schmidt-Fellner, A. Kayser: Proceedings of ASME GT2006, Barcellona (2006), ASME paper GT2006-90473, p.1.

5. K.Y. Sanliturk, M. Imregun, D.J. Ewins: Journal of Vibration and Acoustics, Vol. 119 (1997), p.96.

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