Abstract
Experiments investigating earthquake response of structures traditionally use conventional wired instruments such as strain gauges, displacement transducers, and accelerometers deployed at key areas of interest throughout structure. for wind turbines the rotor is one of these key areas, but due to rotation it is not possible to use wired instruments without a special slip ring. in a recent experiment conducted using the Network for Earthquake Engineering Simulation (NEES) Large High Performance Shake Table (LHPOST) at the University of California, San Diego (UCSD) the global response of a full scale 65-kW turbine (22 m hub height) was monitored using a novel combination of traditional instrumentation in conjunction with point tracking videogrammetry. using this approach, conventional strain, displacement, and acceleration instruments monitored the response of the turbine tower, and the rotor was monitored by observing 16 target points placed on each blade which successfully provided insight not previously available for the global response of a turbine to earthquake shaking while spinning. Excellent correlation was observed between the conventional measurements and results from videogrammetry. This paper presents the methodology used and key response parameters. Such information is extremely valuable for validation of numerical simulation of combined earthquake and wind loads for wind turbines. Copyright © 2011 by Ian Prowell.
Recommended Citation
I. Prowell et al., "Measuring Global Response of a Wind Turbine to Simulated Earthquake Shaking Assisted by Point Tracking Videogrammetry," Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, article no. AIAA 2011-1946, American Institute of Aeronautics and Astronautics, Dec 2011.
The definitive version is available at https://doi.org/10.2514/6.2011-1946
Department(s)
Civil, Architectural and Environmental Engineering
Publication Status
Full Access
International Standard Book Number (ISBN)
978-160086951-8
International Standard Serial Number (ISSN)
0273-4508
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2024 American Institute of Aeronautics and Astronautics, All rights reserved.
Publication Date
01 Dec 2011
Comments
National Science Foundation, Grant None