Publication | Closed Access
A Method for Determination of Damping for Edgewise Blade Vibrations
92
Citations
1
References
2000
Year
EngineeringMechanical EngineeringEdgewise Blade VibrationsComputational MechanicsWind Turbine AerodynamicsWind EngineeringVibrationsWind TurbinesNonlinear Vibration ControlVibration IsolationStructural DynamicEffective DampingStructural VibrationStructural Health MonitoringActive Vibration ControlWind Turbine ModelingAerospace EngineeringWind Turbine BladesMechanical SystemsAeroelasticityAerodynamicsWind Energy TechnologyStructural MechanicsVibration Control
Abstract Violent edgewise blade vibrations have in recent years been a large problem for some stall‐regulated wind turbines. Owing to the complexity of the phenomenon, it has been difficult to predict the risk of these vibrations with aeroelastic load prediction tools. One problem is the choice of parameters in the aeroelastic model, e.g. structural damping and aerodynamic aerofoil characteristics. In many cases a high degree of uncertainty in the predicted response exists and the need for experimental verification methods is obvious. In this work a new method to identify the effective damping for the edgewise blade mode shape for wind turbines has been developed. The method consists of an exciter mechanism which makes it possible to excite the edgewise blade mode shapes from the wind turbine nacelle. Furthermore, the method consists of an analysis method which enables a straightforward determination of the damping. The analysis method is based on a local blade whirl description of the edgewise blade vibrations. The method is verified on a Bonus wind turbine, and for this specific turbine the effective damping for edgewise blade vibrations has been determined. The results support the further development of aeroelastic models and show potential for fine‐tuning of parameters of importance for the edgewise blade vibration problem. Furthermore, the method can be used for experimental investigation of the risk of edgewise blade vibrations for a specific turbine. Copyright © 2000 John Wiley & Sons, Ltd.
| Year | Citations | |
|---|---|---|
Page 1
Page 1