modal dynamics of wind turbines with anisotropic rotors peter f. skjoldan 7 january 2009
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Modal Dynamics of Wind Turbines with Anisotropic Rotors Peter F. Skjoldan 7 January 2009. Presentation. Ph.D. project ”Aeroservoelastic stability analysis and design of wind turbines” Collaboration between Siemens Wind Power A/S Risø DTU - National Laboratory for Sustainable Energy. Outline. - PowerPoint PPT PresentationTRANSCRIPT
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Modal Dynamics of Wind Turbines with Anisotropic RotorsPeter F. Skjoldan7 January 2009
2009-01-07 2/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Presentation
Ph.D. project ”Aeroservoelastic stability analysis and design of wind turbines”
Collaboration between
Siemens Wind Power A/S
Risø DTU - National Laboratory for Sustainable Energy
2009-01-07 3/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Outline
Motivations
Wind turbine model
Modal analysis
Results for isotropic rotor
Analysis methods for anisotropic rotor
Results for anisotropic rotor
Conclusions and future work
2009-01-07 4/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Motivations
Far goal: build stability tool compatible with aeroelastic model used in industry
Conventional wind turbine stability tools consider isotropic conditions
Load calculations are performed in anisotropic conditions
Method of Coleman transformation works only in isotropic conditions
Alternative 1: Floquet analysis
Alternative 2: Hill’s method
Effect of anisotropy on the modal dynamics
2009-01-07 5/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Model of wind turbine
3 DOF on rotor (blade flap), 2 DOF on support (tilt and yaw)
Structrual model (no aerodynamics), no gravity
Blade stiffnesses can be varied to give rotor anisotropy
2009-01-07 6/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Modal analysis
Modal analysis of wind turbine in operation
Operating point defined by a constant mean rotor speed
Time-invariant system needed for eigenvalue analysis
Coordinate transformation to yield time-invariance
Modal frequencies, damping, eigenvectors / periodic mode shapes
Describes motion for small perturbations around operating point
2009-01-07 7/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Floquet theory
Solution to a linear system with periodic coefficients:
periodic mode shape oscillating term
Describes solution form for all methods in this paper
2009-01-07 8/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Coleman transformation
Introduces multiblade coordinates on rotor
Describes rotor as a whole in the inertial frame instead of individual blades in the rotating frame
Yields time-invariant system if rotor is isotropic
Modal analysis performed by traditional eigenvalue analysis of system matrix
2009-01-07 9/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Results for isotropic rotor
1st forward whirling modal solution
Time domain Frequency domain
2009-01-07 10/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Floquet analysis
Numerical integration of system equations gives fundamental solution and monodromy matrix
Lyapunov-Floquet transformation yields time-invariant system
Modal frequencies and damping found from eigenvalues of Rwith non-unique frequency
Periodic mode shapes
2009-01-07 11/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Hill’s method
Solution form from Floquet theory
Fourier expansion of system matrix and periodic mode shape(in multiblade coordinates)
Inserted into equations of motion
Equate coefficients of equal harmonic terms
2009-01-07 12/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Hill’s method
Hypermatrix eigenvalue problem
2009-01-07 13/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Hill’s method
Eigenvalues of hypermatrix
Multiple eigenvalues for each physical mode
2 additional harmonic terms(n = 2)
2009-01-07 14/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Identification of modal frequency
Non-unique frequencies and periodic mode shapes
Modal frequency is chosen such that the periodic mode shape isas constant as possible in multiblade coordinates
j j
Amplitude
Amplitude
Floquet analysis Hill’s method
n = 2
2009-01-07 15/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Comparison of methods
Convergence of eigenvalues
Floquet analysis Hill’s method
2009-01-07 16/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Comparison of methods
Floquet analysis:Mode shapes in time domain
+ Nonlinear model can be used directly to provide fundamental solutions– Slow (numerical integration)
Hill’s method:Mode shapes in frequency domain
+ Fast (pure eigenvalue problem)+ Accuracy increased by using Coleman transformation– Eigenvalue problem can be very large
Frequency non-uniqueness can be resolved using a common approach
2009-01-07 17/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Results for anisotropic rotor
Blade 1 is 16% stiffer than blades 2 and 3
Small change in frequencies compared to isotropic rotor
Larger effect on damping of some modes
Mode 1st BW 1st FW Symmetric 2nd yaw 2nd tilt
Frequency, Hz 0.447 0.749 0.860 1.471 1.590
Deviation from isotropic case, % 0.20 0.41 0.45 0.03 0.006
Damping, s-1 0.0101 0.0125 0.0127 0.0733 0.0681
Deviation from isotropic case, % 4.1 0.36 2.7 0.08 0.03
2009-01-07 18/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Results for anisotropic rotor
1st backward whirling mode, Fourier coefficients
Blade 116% stiffer thanblades 2 and 3
2009-01-07 19/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Results for anisotropic rotor
Symmetric mode, Fourier coefficients
Blade 116% stiffer thanblades 2 and 3
2009-01-07 20/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Results for anisotropic rotor
2nd yaw mode, Fourier coefficients
Blade 116% stiffer thanblades 2 and 3
2009-01-07 21/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Conclusions
Isotropic rotor: Coleman transformation yields time-invariant systemMotion with at most three harmonic components
Anisotropic rotor: Floquet analysis or Hill’s methodMotion with many harmonic components
These methods give similar resultsFrequency non-uniqueness resolved using a common approach
Anisotropy affects some modes more:whirling / low damping / low frequency ?
Additional harmonic components on anisotropic rotor are smallbut might have significant effect when coupled to aerodynamics
2009-01-07 22/22Modal Dynamics of Wind Turbines with Anisotropic Rotors, Peter F. Skjoldan
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Further work
Set up full finite element model and obtain linearized system
Apply Floquet analysis or Hill’s method to full model
Compare anisotropy in the rotating frame (rotor imbalance) and in the inertial frame (wind shear, yaw/tilt misalignment, gravity, tower shadow)