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Application of Genetic Algorithm for Synthesis of H∞ Controllers for Active Magnetic Bearing Systems Read chapter Read first chapter

2019 | OriginalPaper | Chapter

Modal Testing of a Full-Scale Rotating Woven Composite Fan Using Piezoelectric Excitation

Authors : Antoine Mabilia, Claude Gibert, Fabrice Thouverez, Edouard De Jaeghere, Lionel Sanchez, Laura Giovannoni

Published in: Proceedings of the 10th International Conference on Rotor Dynamics – IFToMM

Publisher: Springer International Publishing

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Abstract

An experimental facility for testing full-scale bladed disks in vacuum conditions and under centrifugal load is described in this paper. The special feature of the PHARE#1 test rig is its multichannel excitation system which allows to excite woven composite fan blades with any spatial and phase distribution as well as synchronous or non-synchronous vibration forcing with respect to rotation speed. The configuration of the excitation system allows each blade to be excited independently and therefore nodal diameter excitations can be performed with traveling (forward, backward or mixed) or standing waves. First rotations of the PHARE#1 test rig produced results at different rotation speeds, for several modes, nodal diameters and excitation levels. Typical results analysis and findings are presented in this paper.

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previous chapter Auto Resonance Based Identification of Rotating Systems
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Literature
1.
Gibert, C., Kharyton, V., Thouverez, F., Jean, P.: On forced response of a rotating integrally bladed disk: predictions and experiments. In: ASME Paper No. GT2010-23610 (2010)
2.
Kielb, J.J., Abhari, R.S., Dunn, M.G.: Experimental and numerical study of forced response in a full-scale rotating turbine. In: ASME Paper (2001)
3.
Belz, J., May, M., Siemann, J., Seume, J.R., Voigt, C., Böhmer, H., Grüber, B.: Excited blade vibration for aeroelastic investigations of a rotating blisk using piezoelectric macro fiber composites. In: Proceedings of the ASME Turbo Expo 2013: Power for Land, Sea and Air (2013)
4.
Goltz, I., Böhmer, H., Nollau, R., Belz, J., Grüber, B., Seume, J.: Piezo-electric actuation of rotor blades in an axial compressor. In: ETC 2009 - 8th European Conference on Turbomachinery (2009)
5.
Almeida, P., Gibert, C., Thouverez, F., Leblanc, X., Ousty, J.P.: Experimental analysis of dynamic interaction between a centrifugal compressor and its casing. J. Turbomach. 137(3), 031008 (2015)CrossRef
6.
Padova, C., Barton, J., Dunn, M.G., Manwaring, S., Young, G., Adams, M., Adams, M.: Development of an experimental capability to produce controlled blade tip/shroud rubs at engine speed. J. Turbomach. 127(4), 726–735 (2005)CrossRef
7.
Millecamps, A., Brunel, J.F., Dufrénoy, P., Garcin, F., Nucci, M.: Influence of thermal effects during blade-casing contact experiments. In: ASME Paper No. DETC2009-86842 (2009)
8.
Jacquet-Richardet, G., Torkhani, M., Cartraud, P., Thouverez, F., Baranger, T.N., Herran, M., Gibert, C., Baguet, S., Almeida, P., Peletan, L.: Rotor to stator contacts in turbomachines. Review and application. Mech. Syst. Sig. Process. 40(2), 401–420 (2013)CrossRef
9.
Charleux, D., Gibert, C., Thouverez, F., Dupeux, J.: Numerical and experimental study of friction damping blade attachments of rotating bladed disks. Int. J. Rotat. Mach. 2006, 13 p. (2006). Article ID 71302
10.
Jean, P., Gibert, C., Dupont, C., Lombard, J.P.: Test-model correlation of dry-friction damping phenomena in aero-engines. In: ASME Turbo Expo 2008: Power for Land, Sea, and Air. American Society of Mechanical Engineers (2008)
11.
Laxalde, D., Gibert, C., Thouverez, F.: Experimental and numerical investigations of friction rings damping of blisks. In: ASME Paper No. GT2008-50862 (2008)
12.
Szwedowicz, J., Gibert, C., Sommer, T., Kellerer, R.: Numerical and experimental damping assessment of a thin-walled friction damper in the rotating setup with high pressure turbine blades. J. Eng. Gas Turbines Power 130(1), 012502 (2008)CrossRef
13.
Zhou, B., Thouverez, F., Lenoir, D.: Essentially nonlinear piezoelectric shunt circuits applied to mistuned bladed disks. J. Sound Vib. 333(9), 2520–2542 (2014)CrossRef
14.
Choi, B., Kauffman, J., Duffy, K., Provenza, A., Morrison, C.: Active vibration reduction of titanium alloy fan blades (FAN1) using piezoelectric materials. In: Propulsion-Safety and Affordable Readiness (P-SAR) Conference (2010)
15.
Botta, F., Marx, N., Gentili, S., Schwingshackl, C., Mare, L.D., Cerri, G., Dini, D.: Optimal placement of piezoelectric plates for active vibration control of gas turbine blades: experimental results. In: Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems, vol. 8345. International Society for Optics and Photonics (2012)
16.
Dambrine, B., Molinari, O., Coupe, D.: Turbomachine blade, in particular a fan blade, and its method of manufacture. US Patent 7,241,112 B2 (2007)
17.
ANSI/IEEE: IEEE standard on piezoelectricity. IEEE Standard 176-1987 (1987)
18.
Duffy, K.P., Choi, B.B., Provenza, A.J., Min, J.B., Kray, N.: Active piezoelectric vibration control of subscale composite fan blades. J. Eng. Gas Turbines Power 135(1), 011601 (2013)CrossRef
19.
Judge, J., Pierre, C., Mehmed, O.: Experimental investigation of mode localization and forced response amplitude magnification for a mistuned bladed disk. In: ASME Turbo Expo 2000: Power for Land, Sea, and Air. American Society of Mechanical Engineers (2000)
20.
Gloth, G., Sinapius, M.: Analysis of swept-sine runs during modal identification. Mech. Syst. Sig. Process. 18(6), 1421–1441 (2004)CrossRef
21.
Ozdemir, A.A., Gumussoy, S.: Transfer function estimation in system identification toolbox via vector fitting. IFAC-PapersOnLine 50(1), 6232–6237 (2017)CrossRef
22.
Ewins, D.J.: Modal Testing: Theory and Practice, vol. 15. Research Studies Press, Letchworth (1984)
23.
Joannin, C., Chouvion, B., Thouverez, F., Ousty, J.P., Mbaye, M.: A nonlinear component mode synthesis method for the computation of steady-state vibrations in non-conservative systems. Mech. Syst. Sig. Process. 83, 75–92 (2017)CrossRef
Metadata
Title
Modal Testing of a Full-Scale Rotating Woven Composite Fan Using Piezoelectric Excitation
Authors
Antoine Mabilia
Claude Gibert
Fabrice Thouverez
Edouard De Jaeghere
Lionel Sanchez
Laura Giovannoni
Copyright Year
2019
Book
Proceedings of the 10th International Conference on Rotor Dynamics – IFToMM

Print ISBN: 978-3-319-99269-3

Electronic ISBN: 978-3-319-99270-9

Copyright Year: 2019

DOI
https://doi.org/10.1007/978-3-319-99270-9_21

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