Micropower from Tidal Turbines



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Transcription:

Micropower from Tidal Turbines Brian Polagye 1, Rob Cavagnaro 1, and Adam Niblick 2 1 Northwest National Marine Renewable Energy Center, University of Washington 2 Creare, Inc. 13th International Symposium on Fluid Power July 9, 2013

Tidal Current Energy Utility scale (> 1 MW) turbines harnessing renewable, predictable kinetic energy from tidal currents Siemens/MCT Ocean Renewable Power Company Andritz Hydro/Hammerfest

Physical environment: Near field Physical environment: Far field Habitat Invertebrates Potential Environmental Impacts Device presence: Static effects Device presence: Dynamic effects Chemical effects Acoustic effects Electromagnetic effects Energy removal Cumulative effects Low Moderate High Scientific Uncertainty Potential Significance Low Moderate Fish: Migratory Fish: Resident Marine mammals Seabirds High Polagye, B., B. Van Cleve, A. Copping, and K. Kirkendall (eds), (2011) Environmental effects of tidal energy development. Ecosystem interactions

Studying Changes to Distribution and Use Pre installation studies of tidal energy sites must typically rely on autonomous instrumentation Active acoustic sensors for observations of marine life have relatively high power draws (> 20 W) 3 4 deep cycle lead acid batteries required to achieve 10% duty cycle for 1 month SoundMetrics DIDSON BioSonics DTX

Tidal Micropower Concept Support Frame Turbine Generator and Battery Storage Integrate energy harvesting capability into sensor package Modular alternative to cabled observatories Target 10 20 W/m 2 power output (including battery storage losses)

System Components Kinetic Power Rotor Mechanical Power Power Train Electrical Power Controller P 1 2 U 3 AC P o Battery Storage Flow Velocity Swept Area Balance of System Efficiency Sensors Rotor Efficiency

Micropower Rotor Requirements Self starting without external excitation Accommodate currents with time varying direction High efficiency conversion of kinetic power to electrical power

Rotor Selection Cross flow turbine High solidity Helical blades NACA 0018 profile N: Number of blades (4) H/D: Aspect Ratio (1.4) φ: Blade helix angle (60 o ) Nc σ: Turbine solidity (0.3) D Limited existing parametric studies Shiono, M., Suzuki, K., and Kiho, S., 2002, Output characteristics of Darrieus water turbine with helical blades for tidal current generations, Proceedings of the Twelfth International Offshore and Polar Engineering Conference, Kitakyushu, Japan, pp. 859 864. Bachant, P., and Wosnik, M. 2011, Experimental investigation of helical cross flow axis hydrokinetic turbines, including effects of waves and turbulence, Proceedings of the ASME JSME KSME 2011 Joint Fluids Engineering Conference, Hamamatsu, Shizuoka, Japan.

Principle of Operation Radius Rotational rate R U Free stream Velocity U 1 2 1 2 cos 2 Neglecting wake and induction Local Velocity

Laboratory Experiments Chord Length Re Uc Re c 3 5 10 10 Blockage Ratio 18 21% Froude number Fr 0.2 0.4 Turbulence Intensity U I 4% U Niblick, A.L., 2012, Experimental and analytical study of helical crossflow turbines for a tidal micropower generation system, Masters thesis, University of Washington, Seattle, WA.

Turbine Operation

C p λ Velocity Dependence Whelan, J. I., J. M. R. Graham, and J. Peiro (2009) A freesurface and blockage correction for tidal turbines. Journal of Fluid Mechanics 624, 1: 281 291.

Possible Effect of Reynolds Number Approximate Local Velocity Re c Uc 3 5 10 10 Sheldahl, R. E. and Klimas, P. C., 1981, Aerodynamic characteristics of seven airfoil sections through 180 degrees angle of attack for use in aerodynamic analysis of vertical axis wind turbines, SAND80 2114, March 1981, Sandia National Laboratories, Albuquerque, New Mexico.

Angle of Attack Variation Angular Position sin tan 1 cos Tip Speed Ratio

Significance of Dynamic Stall Range of α at position of maximum torque along each blade 4 Re c 5x10 Jacobs, E.N., and Sherman, A., 1937, Airfoil section characteristics as affected by variations of the Reynolds number, Report No. 586, National Advisory Committee for Aeronautics.

Tow vessel Field Experiments Tow line (~100 m) Skiff (w/ load bank) Skiff Attachment Generator Gearbox Re c U I U 4 5 10 10 4% Rotor 0% Fr 0 No Blockage

Turbine Operation

Electrical Power Field Performance C Pe U RH P o 3? Radius Height

Laboratory Dynamometer Reaction Torque Sensor Generator Encoder Coupling to Motor Generator connected to field testing load bank Motor driven by variable frequency drive (3 phase AC) Evaluate generator and gearbox efficiency under same conditions as field test (loads and rpm)

Generator Efficiency

Gearbox Efficiency

Field Performance System Performance Rotor Performance Rotor performance (without blockage) in line with expectations from prior work by Bachant and Wosnik (2011), accounting for higher solidity

Response to Turbulent Perturbations G f S P e P e S PP f f f c U L Taylor s hypothesis f c 2 Hz Smallest engulfing gust U 1.5m/s Maximum C P

Tidal Micropower Feasibility Self starting without external excitation Accommodate currents with time varying direction High efficiency conversion of kinetic power to electrical power Low balance of system efficiency Relatively low rotor efficiency

Improved Rotor Efficiency Design Refinements Decrease solidity to increase λ Asymmetric foil with higher C L /C D at Re c ~ 10 4 10 5 (similar Re c to UAVs) Submersible Direct Drive Generator With existing drivetrain, optimal λ depends on inflow velocity (undesirable for control) Eliminate rotary seal Minimize thermal management challenge http://adg.stanford.edu/aa241/airfoils/air foilhistory.html

Acknowledgements This material is based upon work supported by the Department of Energy under Award Number DE FG36 08GO18179. Funding for field scale turbine fabrication and testing provided by the University of Washington Royalty Research Fund. Fellowship support for Adam Niblick and Robert Cavagnaro was provided by Dr. Roy Martin. Two senior level undergraduate Capstone Design teams fabricated the turbine blades and test rig. Martin Wosnik and Pete Bachant provided a number of helpful comments on representations of the blade chord Reynolds number for cross flow turbines.