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Dual-Actuator Active Vibration-Control SystemDual-actuator active vibration-control (DAAVC) system is developmental system of type described in "Active Vibration Dampers for Rotating Machinery" (LEW-15427). System features sensors and actuators positioned and oriented at bearings to measure and counteract vibrations of shaft along either of two axes perpendicular to axis of rotation. Effective in damping vibrations of helicopter-engine test stand, making it safer to operate engine at speeds near and above first resonance of engine/test-stand system. Opens new opportunities for engine designers to draw more power from engine, and concept applicable to other rotating machines.
Document ID
19940000696
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kascak, Albert F.
(NASA Lewis Research Center, Cleveland, OH.)
Kiraly, Louis J.
(NASA Lewis Research Center, Cleveland, OH.)
Montague, Gerald T.
(Sverdrup Technology, Inc.)
Palazzolo, Alan B.
(Texas A&M Univ.)
Manchala, Daniel
(Texas A&M Univ.)
Date Acquired
August 16, 2013
Publication Date
December 1, 1994
Publication Information
Publication: NASA Tech Briefs
Volume: 18
Issue: 12
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-15765
Accession Number
94B10696
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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