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PZT Active Frequency Based Wind Blade Fatigue to Failure Testing Results for Various Blade Designs

R. J. WERLINK

Abstract


This paper summarizes NASA PZT Health Monitoring System results previously reported for 9 meter blade Fatigue loading to failure conducted at The National Renewable Energy Lab Wind blade testing facility results using the on the CX-100, TX-100 and BSDS designs. A collaborative effort between Sandia National Laboratories (SNL) and NASA KSC has been performed to evaluate the viability of a NASA Developed PZT Piezoelectric sensor/actuator for structural health monitoring (SHM) of Wind turbine blades. The innovation behind the NASA developed sensors in the combination of signal data processing with the development of a unique sensor/actuator consisting of piezoelectric materials in a thin and highly sensitive configuration. This paper summarizes previous NASA PZT system testing and includes results of the Fatigue testing of a 9 Meter Wind blade fatigue test referred to as the Sensor Blade which was based on the CX-100 design. This configuration had internal instrumentation/video and consisted of an internal manufacturing known defect. The defect provided an opportunity to demonstrate the PZT Health monitoring performance.

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