Grants and Contracts Details
Description
Improvement in aerodynamic performance in turbomachinery can significantly enhance
power generation efficiency. Turbomachinery involves rotor blades (blades which rotate)
and stator vanes (blades which do not rotate). A primary goal in blade design is
optimization of aerodynamic performance. Often, however, a blade design optimized for
aerodynamic performance is not acceptable because structural analysis predicts large
amplitude vibration response, which can result in fatigue failure. So, design modifications
are necessary, which may compromise aerodynamic performance. Therefore, it is
desirable to develop techniques to control blade vibratory response without significantly
altering blade shape. One method involves mounting "smart materials", such as
piezoelectric patches, on blades for control actuation to counteract vibrations. A research
project at the University of Kentucky is currently underway in which the vibratory
response of a stator vane has been reduced significantly in the UK Low Speed Research
Compressor using piezoelectric patches. The proposed work would extend this research
to develop methods for also minimizing the vibratory response of the rotating blades.
There are significant challenges in controlling vibrations of rotating blades. The control is
based on feedback of measured response of the vibrating blade. The response is measured
through a voltage signal from a sensor, such as an accelerometer. For a stator vane, it is
simple to feed wiring ITom sensors to a data acquisition unit. For a rotating blade,
however, the sensor signal and control signal must be fed through a slip ring, adding a
level of complexity to the system. Verification is needed that this can be accomplished
without significant reduction in control effectiveness. It is likely that electrical noise will
be introduced by the slip ring. Further, smart materials on a rotating blade will experience
centrifugal forces, and best methods for mounting need to be determined to prevent the
materials from separating from the blades.
Status | Finished |
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Effective start/end date | 11/1/05 → 2/28/07 |
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