The simulations indicated the potential of active casings to modify the blade tip clearance enough to improve stage efficiency. They also provided valuable design information, such as preliminary actuator configurations (number and location) and the corresponding voltage patterns required to compensate for uneven casing deformations. The figure illustrates an active ovalization of a casing with four discrete piezoceramic actuators attached on the outer surface. The center figure shows the predicted radial displacements along the hoop direction that are induced when electrostatic voltage (bottom figure) is applied at the piezoceramic actuators. This work, which has demonstrated the capabilities of in-house computational models to analyze and design active casing structures, is expected to contribute toward the development of advanced subsonic engines.

Active ring structures with piezoelectric actuators. Top: Typical configuration. Center: Induced radial deflections. Bottom: Applied electric voltage at actuators .
Saravanos, D.A., et al.: On Smart Composite Structures for Active Tip Clearance Control. Adaptive Structures and Composite Materials Analysis and Application. E. Garcia, H. Cudney, and A. Dasgupta, eds., ASME, New York, 1994.
Last updated April 26, 1996
Responsible NASA Official:
Gynelle.C.Steele@nasa.gov
216-433-8258
Point of contact for NASA Glenn's Research & Technology reports:
Cynthia.L.Dreibelbis@nasa.gov
216-433-2912
SGT, Inc.
Web page curator:
Nancy.L.Obryan@nasa.gov
216-433-5793
Wyle Information Systems, LLC