Bifurcation and dynamic response analysis of rotating blade excited by upstream vortices

A reduced model is proposed and analyzed for the simulation of vortex-induced vibrations (VIVs) for turbine blades. A rotating blade is modelled as a uniform cantilever beam, while a van der Pol oscillator is used to represent the time-varying characteristics of the vortex shedding, which interacts with the equations of motion for the blade to simulate the fluid-structure interaction. The action for the structural motion on the fluid is considered as a linear inertia coupling. The nonlinear characteristics for the dynamic responses are investigated with the multiple scale method, and the modulation equations are derived. The transition set consisting of the bifurcation set and the hysteresis set is constructed by the singularity theory and the effects of the system parameters, such as the van der Pol damping. The coupling parameter on the equilibrium solutions is analyzed. The frequency-response curves are obtained, and the stabilities are determined by the Routh-Hurwitz criterion. The phenomena including the saddle-node and Hopf bifurcations are found to occur under certain parameter values. A direct numerical method is used to analyze the dynamic characteristics for the original system and verify the validity of the multiple scale method. The results indicate that the new coupled model is useful in explaining the rich dynamic response characteristics such as possible bifurcation phenomena in the VIVs.

[1]  Cyril Touzé,et al.  Nonlinear forced vibrations of thin structures with tuned eigenfrequencies: the cases of 1:2:4 and 1:2:2 internal resonances , 2014 .

[2]  Jan R. Wright,et al.  BLADE-TIP TIMING MEASUREMENT OF SYNCHRONOUS VIBRATIONS OF ROTATING BLADED ASSEMBLIES , 2002 .

[3]  Bifurcation analysis of a double pendulum with internal resonance , 2000 .

[4]  O. M. Griffin,et al.  A model for the vortex-excited resonant response of bluff cylinders , 1973 .

[5]  J. Lai,et al.  Jet characteristics of a plunging airfoil , 1999 .

[6]  Carl M. Larsen,et al.  Direct Numerical Simulation and Experimental Investigation on Suppression of Vortex Induced Vibrations of Circular Cylinders by Radial Water Jets , 2003 .

[7]  Wei Shyy,et al.  Flapping and flexible wings for biological and micro air vehicles , 1999 .

[8]  C. H. Sieverding,et al.  The Influence of Boundary Layer State on Vortex Shedding from Flat Plates and Turbine Cascades , 1989 .

[9]  Hongxiang Xue,et al.  Simplified model for evaluation of VIV-induced fatigue damage of deepwater marine risers , 2009 .

[10]  Zhifeng Hao,et al.  Two-sided damping constraint control strategy for high-performance vibration isolation and end-stop impact protection , 2016 .

[11]  J. S. Rao,et al.  Turbomachine blade damping , 2003 .

[12]  M. A. Barron-Meza Vibration Analysis Of a Self-Excited Elastic Beam , 2010 .

[13]  A. Tondl,et al.  Non-linear Vibrations , 1986 .

[14]  Ilmar F. Santos,et al.  Frequencies in the Vibration Induced by the Rotor Stator Interaction in a Centrifugal Pump Turbine , 2007 .

[15]  Haym Benaroya,et al.  An overview of modeling and experiments of vortex-induced vibration of circular cylinders , 2005 .

[16]  Emmanuel de Langre,et al.  Vortex-induced travelling waves along a cable , 2004 .

[17]  I. G. Currie,et al.  Lift-Oscillator Model of Vortex-Induced Vibration , 1970 .

[18]  Xiaodong Wang,et al.  Nonlinear dynamic singularity analysis of two interconnected synchronous generator system with 1:3 internal resonance and parametric principal resonance , 2015 .

[19]  M. Wiercigroch,et al.  A Reduced Order Model for Vortex–Induced Vibration of a Vertical Offshore Riser in Lock–in , 2008 .

[20]  Pascal Hémon,et al.  AN IMPROVEMENT OF THE TIME DELAYED QUASI-STEADY MODEL FOR THE OSCILLATIONS OF CIRCULAR CYLINDERS IN CROSS-FLOW , 1999 .

[21]  Yi-Ze Wang,et al.  Nonlinear primary resonance of nano beam with axial initial load by nonlocal continuum theory , 2014 .

[22]  Régis Lengellé,et al.  Nonintrusive turbomachine blade vibration measurement system , 2007 .

[23]  A. Roshko,et al.  Vortex formation in the wake of an oscillating cylinder , 1988 .

[24]  Qingjie Cao,et al.  A three-degree-of-freedom model for vortex-induced vibrations of turbine blades , 2016 .

[25]  P. Cochat,et al.  Et al , 2008, Archives de pediatrie : organe officiel de la Societe francaise de pediatrie.

[26]  Qingjie Cao,et al.  Bifurcation analysis for vibrations of a turbine blade excited by air flows , 2016 .

[27]  Mihir Sen,et al.  Synchronization of coupled self-excited elastic beams , 2009 .

[28]  Alexander F. Vakakis,et al.  Suppression of limit cycle oscillations in the van der Pol oscillator by means of passive non‐linear energy sinks , 2006 .

[29]  Charles H. K. Williamson,et al.  A brief review of recent results in vortex-induced vibrations , 2008 .

[30]  Richard Evelyn Donohue Bishop,et al.  The lift and drag forces on a circular cylinder in a flowing fluid , 1964, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[31]  John Young,et al.  Oscillation Frequency and Amplitude Effects on the Wake of a Plunging Airfoil , 2004 .

[32]  Dong Wei,et al.  Nonlinear vibration characteristics of a flexible blade with friction damping due to tip-rub , 2011 .

[33]  R. Clough,et al.  Dynamics Of Structures , 1975 .

[34]  Sanford S. Davis,et al.  Visualization of Quasiperiodic Flows , 1979 .

[35]  Gökhan Bulut,et al.  On nonlinear vibrations of a rotating beam , 2009 .

[36]  Christophe Pierre,et al.  Modal Reduction of a Nonlinear Rotating Beam Through Nonlinear Normal Modes , 2002 .

[37]  R. Violette,et al.  Computation of vortex-induced vibrations of long structures using a wake oscillator model: Comparison with DNS and experiments , 2007 .

[38]  Marian Wiercigroch,et al.  Reduced-order modelling of vortex-induced vibration of catenary riser , 2009 .

[39]  C. H. Sieverding,et al.  The Influence of Boundary Layer State on Vortex Shedding From Flat Plates and Turbine Cascades , 1989 .

[40]  Max F. Platzer,et al.  On Vortex Formation in the Wake Flows of Transonic Turbine Blades and Oscillating Airfoils , 2006 .

[41]  Ranjan Ganguli,et al.  Monitoring low cycle fatigue damage in turbine blade using vibration characteristics , 2007 .

[42]  E. de Langre,et al.  Coupling of Structure and Wake Oscillators in Vortex-Induced Vibrations , 2004 .

[43]  R. Skop,et al.  A new twist on an old model for vortex-excited vibrations , 1997 .

[44]  M. Koochesfahani Vortical patterns in the wake of an oscillating airfoil , 1987 .

[45]  Emmanuel Guilmineau,et al.  Numerical simulation of vortex-induced vibration of a circular cylinder with low mass-damping in a turbulent flow , 2004 .

[46]  Yushu Chen,et al.  Singularity analysis of a two-dimensional elastic cable with 1:1 internal resonance , 2010 .

[47]  Shupeng Sun,et al.  Impact vibration characteristics of a shrouded blade with asymmetric gaps under wake flow excitations , 2013 .

[48]  Andrew Y. T. Leung,et al.  Bifurcation and Chaos in Engineering , 1998 .

[49]  Hideo Ohashi,et al.  Visualization Study of Flow Near the Trailing Edge of an Oscillating Airfoil , 1972 .

[50]  E. de Langre,et al.  Vortex shedding modeling using diffusive van der Pol oscillators , 2002 .

[51]  Zhifeng Hao,et al.  The isolation characteristics of an archetypal dynamical model with stable-quasi-zero-stiffness , 2015 .