Skip to main content
Log in

On the occurrence of self-synchronization of autooscillations of turbocompressor rotor blades

  • Machine Mechanics
  • Published:
Journal of Machinery Manufacture and Reliability Aims and scope Submit manuscript

Abstract

The self-synchronization of the spectral parameters of turbocompressor blades is studied, as well as its connection with nonlinear resonance during fluttering. The evolution of blade oscillations during the growth of turbocompressor rotor revolutions is characterized by the concurrence of torsional and flexural oscillation modes, a change of the base frequencies of the rotor blades, and the appearance of a common synchronization frequency in their spectrum. Fluttering comes with a loss of stability of the blades’ oscillation mode at the synchronization frequency. Estimates are obtained on the basis of the spectral analysis of the recording of transient processes of axial and centrifugal turbocompressors. The parameters of the blade oscillation modes and their power have been identified by means of the construction of models of the processes on the basis of the technology of Proni spectral analysis.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. Ganiev, R.F. and Koval’chuk, P.S., Dinamika sistem tverdykh i uprugikh tel (Dynamics of Solids and Elastic Bodies), Moscow: Mashinostroenie, 1980.

    Google Scholar 

  2. Ganiev, R.F. and Fazullin, F.F., On Synchronization Problems of Mechanical Systems with Round Symmetry, Dokl. Akad. Nauk UkSSR. Ser. A, 1976, no. 11, pp. 92–97.

  3. Whitehead, D.S., Force and Moment Coefficients for Vibrating Airfoils in Cascade. Reports and Memoranda 3254, London: British Aeronautical Research Council, 1960.

    Google Scholar 

  4. Bendiksen, O.O. and Friedmann, P.P., The Effect of Bending-Torsion Coupling on Fan and Compressor Blade Flutter, Transactions of the ASME, 1982, vol. 104, no. 3, pp. 617–623.

    Google Scholar 

  5. Hall, K.C. and Crawley, E.F., Calculation of Unsteady Flows in Turbomachinery Using the Linearized Euler Equation, AIAA Journal, 1989, vol. 27, no. 6, pp. 777–787.

    Article  Google Scholar 

  6. Whitehead, D.S., Classical Two-Dimensional Methods, in AGARD Manual on Aeroelasticity in Axial-Flow Turbomachines. Vol. 1 Unsteady Turbomachinery Aerodynamics, Paris: AGARD, 1987.

    Google Scholar 

  7. Kielb, J.J. and Abhari, R.S., Experimental Study of Aerodynamic and Structural Damping in Full-Scale Rotating Turbine, Proc. of IGTI: ASME TURBO EXPO 2001, New Orleans, June 4–7 2001.

  8. Bolcs, A. and Fransson, T.H., Aeroelasticity in Turbomachines. Comparison of Theoretical and Experimental Cascade Results, Technical Report TR-870605, Ecole Polytechnique Federale de Lausanne, 1986.

  9. Kaza, K.R.V. and Kielb, R.E., Flutter and Response of a Mistuned Cascade in Incompressible Flow, AIAA Journal, 1982, vol. 20, no. 8, pp. 1120–1127.

    Article  MATH  Google Scholar 

  10. Crawley, E.F. and Hall, K.C., Optimization and Mechanisms of Mistuning in Cascades, Journal of Engineering for Gas Turbines and Power, 1985, vol. 107, no. 2, pp. 418–426.

    Article  Google Scholar 

  11. Imergun, M. and Ewins, D.J., Aeroelastic Vibration Analysis of Tuned and Mistuned Blade Systems, Proc. of Unsteady Aerodynamics of Turbomachines and Propellers Symp., Cambridge: Cambridge University Press, 1984, pp. 149–161.

    Google Scholar 

  12. Balakshin, O.B. and Kukharenko, B.G., Asynchronous Spectral Analysis of Oscillating Time Series, Problemy mashinostroeniya i nadezhnosti mashin, 1996, no. 5, p. 116.

  13. Nowinski, M. and Panovsky, J., Flutter Mechanisms in Low Pressure Turbine Blades, ASME Paper 98-GT-573, American Society of Mechanical Engineers, 1998.

  14. Balakshin, O.B. and Kukharenko, B.G., Spectral Analysis of Turbocompressor’s Blades Flutter, Dokl. RAN, 2007, vol. 417, no. 5, pp. 627–630.

    Google Scholar 

  15. Sadeghi, M. and Liu, F., Computation of Mistuning Effects on Cascade Flutter, AIAA Journal, 2001, vol. 39, no. 1, pp. 22–28.

    Article  Google Scholar 

  16. Balakshin, O.B., Kukharenko, B.G., and Khorikov, A.A., Identification of Turbine Blades Flatter, Problemy mashinostroeniya i nadezhnosti mashin, 2008, no. 1, pp. 19–24.

Download references

Author information

Authors and Affiliations

Authors

Additional information

Original Russian Text © R.F. Ganiev, O.B. Balakshin, B.G. Kukharenko, 2009, published in Problemy Mashinostroeniya i Nadezhnosti Mashin, 2009, No. 6, pp. 16–23.

About this article

Cite this article

Ganiev, R.F., Balakshin, O.B. & Kukharenko, B.G. On the occurrence of self-synchronization of autooscillations of turbocompressor rotor blades. J. Mach. Manuf. Reliab. 38, 535–541 (2009). https://doi.org/10.3103/S105261880906003X

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.3103/S105261880906003X

Keywords

Navigation