Piezoelectric actuators provide an active solution for vibration control in aircraft engines compared to the state-of-the-art squeeze film dampers. The property of piezoelectric materials enable them to be used as sensors and actuators simultaneously. This self-sensing property of the actuator is analyzed in this paper for its ability to detect unbalance faults, which are common in rotor systems. In this paper two different actuator configurations are studied for its ability to diagnose unbalance faults in an aircraft engine. Three parameters of unbalances such as its magnitude, its position in the circumferential and axial direction in a rotor are estimated through simulations. Finally a suitable position to achieve a better fault diagnosis is identified.
Fault Diagnosis on an Aircraft Engine Model Equipped With Self-Sensing Piezoelectric Actuators
- Views Icon Views
- Share Icon Share
- Search Site
Ambur, R, Zhao, X, & Rinderknecht, S. "Fault Diagnosis on an Aircraft Engine Model Equipped With Self-Sensing Piezoelectric Actuators." Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. Volume 7A: Structures and Dynamics. Seoul, South Korea. June 13–17, 2016. V07AT27A006. ASME. https://doi.org/10.1115/GT2016-56975
Download citation file: