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Shunted Piezoelectric Vibration Damping Analysis Including Centrifugal Loading EffectsExcessive vibration of turbomachinery blades causes high cycle fatigue problems which require damping treatments to mitigate vibration levels. One method is the use of piezoelectric materials as passive or active dampers. Based on the technical challenges and requirements learned from previous turbomachinery rotor blades research, an effort has been made to investigate the effectiveness of a shunted piezoelectric for the turbomachinery rotor blades vibration control, specifically for a condition with centrifugal rotation. While ample research has been performed on the use of a piezoelectric material with electric circuits to attempt to control the structural vibration damping, very little study has been done regarding rotational effects. The present study attempts to fill this void. Specifically, the objectives of this study are: (a) to create and analyze finite element models for harmonic forced response vibration analysis coupled with shunted piezoelectric circuits for engine blade operational conditions, (b) to validate the experimental test approaches with numerical results and vice versa, and (c) to establish a numerical modeling capability for vibration control using shunted piezoelectric circuits under rotation. Study has focused on a resonant damping control using shunted piezoelectric patches on plate specimens. Tests and analyses were performed for both non-spinning and spinning conditions. The finite element (FE) shunted piezoelectric circuit damping simulations were performed using the ANSYS Multiphysics code for the resistive and inductive circuit piezoelectric simulations of both conditions. The FE results showed a good correlation with experimental test results. Tests and analyses of shunted piezoelectric damping control, demonstrating with plate specimens, show a great potential to reduce blade vibrations under centrifugal loading.
Document ID
20110016111
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Min, James B.
(NASA Glenn Research Center Cleveland, OH, United States)
Duffy, Kirsten P.
(NASA Glenn Research Center Cleveland, OH, United States)
Provenza, Andrew J.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
April 12, 2011
Subject Category
Mechanical Engineering
Report/Patent Number
E-17955
AIAA Paper 2010-2716
Report Number: E-17955
Report Number: AIAA Paper 2010-2716
Meeting Information
Meeting: 18th AIAA/ASME/AHS Adaptive Structures Conference
Location: Orlando, FL
Country: United States
Start Date: April 12, 2010
End Date: April 15, 2010
Sponsors: American Society of Civil Engineers, American Inst. of Aeronautics and Astronautics, American Helicopter Society, Inc., American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 56158''h,02.08.03.15.13
Distribution Limits
Public
Copyright
Public Use Permitted.
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