Upload
others
View
6
Download
0
Embed Size (px)
Citation preview
Aeroelastic Limit Cycles As A
Small Scale Energy Source
Jared Dunnmon
8th Int. Conf. on Multibody Systems, Nonlinear Dynamics, and Control
Advised by Professor Earl Dowell, Duke University
August 29, 2011
The Idea: Research Concept and Goals
• Utilize aeroelasticallyinduced LCO as a source of energy
• Experimentally investigate capturing energy in the LCO of a cantilevered metal beam with piezoelectric laminates
• Computationally model full “aeroelectroelastic” system behavior
Experimental Methods:
Aeroelectroelastic Beam Experiments
• Self-excited subcritical
LCO occur over a
significant hysteresis band
from 31.5 m/s to 26 m/s
• Normalized amplitudes of
0.46 at 31.5 m/s
• RMS power output of 2.5
mW at 27 m/s
Modeling: Conceptual Framework
• Three dimensional vortex lattice aerodynamic model
• Discontinuous piezoelectric beam electrostructural model
• Experimental natural frequencies and physical parameters input
• In vacuo modeshapes used as an approximation to discontinuous modeshapes
• Essential Mathematics– Bernoulli’s Equation
– Laplace’s Equation
– Velocity Potential-Downwash Boundary Condition
– Hodges-Dowell Equations
Modeling: Basic EquationsCoupled Nonlinear ODEs for Aeroelectroelastic Beam and Electrical Circuit
Full Aeroelectroelastic State Space Equation
State Space Discretization of ODE System and Coupling to Vortex Lattice Aerodynamics
Mass Matrix
Nonlinear Curvature Force
Nonlinear Inertial Forces
Modeling: Basic EquationsCoupled Nonlinear ODEs for Aeroelectroelastic Beam and Electrical Circuit
Full Aeroelectroelastic State Space Equation
State Space Discretization of ODE System and Coupling to Vortex Lattice Aerodynamics
Results: Frequency MeasuresFFT of Experimental Signal FFT of Theoretical Signal
Frequency vs. Amplitude
Results: Power Extraction Measures
Power Extracted vs. Physical Amplitude Power Extracted vs. Resistance (U=27 m/s)
Results: Efficiency Measures
• Capture efficiency estimated by the following equation:
• Remains approximately constant over all observed amplitudes
• Promising potential for a harvester that operates efficiently over a large velocity band
Capture Efficiency vs. Physical Amplitude
Summary: Conclusions and Next Steps
• Conclusions– Rudimentary piezoelectric
aeroelastic energy harvester able to generate significant amounts of power
– Aeroelectroelastic state space model with linear piezoelectric terms approximates system behavior well
– Subcritical LCO potentially desirable for this particular applications
• Next Steps– Optimization
• Electrical components
• Piezoelectric placement
– Advanced Modeling• Wind tunnel walls
• Subcritical LCO
• Advanced electrical network
– New Prototype• Root piezoelectric clamping
• Specialized electronics housing
• SSHI circuit integration
Acknowledgements
Many thanks to the following individuals for their time, effort, and guidance in supporting this project:
Earl Dowell
Deman Tang
Brian Mann
Sam Stanton
Chad Gibbs
Pat McGuire
Casey Dunn
Results: Voltage Linearity Measures
Voltage Amplitude vs. Physical Amplitude Linear Fit of Voltage to Physical Amplitude