The focus of this paper is on demonstrating the potential to damp entire bladed disks using dampers on only a fraction of the blades. This problem is first considered without the presence of random mistuning, and it is demonstrated that a few dampers at optimized locations can lead to a significant reduction in the forced response of the entire bladed disk. Unfortunately, this optimum design may not be robust with respect to random mistuning and a notable fraction of the reduction in forced response obtained may disappear because of mistuning. To regain the reduction in forced response but with mistuning present, robustness to mistuning is enhanced by using intentional mistuning in addition to dampers. The intentional mistuning strategy selected here is the pattern mistuning in which the blades all belong to either type or . An optimization effort is then performed to obtain the best combination of pattern and damper location to minimize the mistuned forced response of the disk. The addition of intentional mistuning in the system is shown to be very efficient, and the optimum bladed disk design does indeed exhibit a significant reduction in mistuned forced response as compared with the tuned system. These findings were obtained on both single-degree-of-freedom per blade-disk models and a reduced order model of a blisk.
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e-mail: javier.avalos@asu.edu
e-mail: marc.mignolet@asu.edu
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September 2010
Research Papers
On Damping Entire Bladed Disks Through Dampers on Only a Few Blades
Javier Avalos,
Javier Avalos
Department of Mechanical and Aerospace Engineering,
e-mail: javier.avalos@asu.edu
Arizona State University
, Tempe, AZ 85287-6106
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Marc P. Mignolet
Marc P. Mignolet
Fellow ASME
Department of Mechanical and Aerospace Engineering,
e-mail: marc.mignolet@asu.edu
Arizona State University
, Tempe, AZ 85287-6106
Search for other works by this author on:
Javier Avalos
Department of Mechanical and Aerospace Engineering,
Arizona State University
, Tempe, AZ 85287-6106e-mail: javier.avalos@asu.edu
Marc P. Mignolet
Fellow ASME
Department of Mechanical and Aerospace Engineering,
Arizona State University
, Tempe, AZ 85287-6106e-mail: marc.mignolet@asu.edu
J. Eng. Gas Turbines Power. Sep 2010, 132(9): 092503 (10 pages)
Published Online: June 7, 2010
Article history
Received:
September 11, 2008
Revised:
September 18, 2008
Online:
June 7, 2010
Published:
June 7, 2010
Citation
Avalos, J., and Mignolet, M. P. (June 7, 2010). "On Damping Entire Bladed Disks Through Dampers on Only a Few Blades." ASME. J. Eng. Gas Turbines Power. September 2010; 132(9): 092503. https://doi.org/10.1115/1.3078792
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