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The use of an optical data acquisition system for bladed disk vibration analysisA new concept in instrumentation was developed by engineers at NASA Lewis Research Center to collect vibration data from multi-bladed rotors. This new concept, known as the optical data acquisition system, uses optical transducers to measure bladed tip delections by reflection light beams off the tips of the blades as they pass in front of the optical transducer. By using an array of transducers around the perimeter of the rotor, detailed vibration signals can be obtained. In this study, resonant frequencies and mode shapes were determined for a 56 bladed rotor using the optical system. Frequency data from the optical system was also compared to data obtained from strain gauge measurements and finite element analysis and was found to be in good agreement.
Document ID
19850006875
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lawrence, C.
(NASA Lewis Research Center Cleveland, OH, United States)
Meyn, E. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1984
Subject Category
Structural Mechanics
Report/Patent Number
E-2358
NAS 1.15:86891
NASA-TM-86891
Report Number: E-2358
Report Number: NAS 1.15:86891
Report Number: NASA-TM-86891
Accession Number
85N15184
Funding Number(s)
PROJECT: RTOP 505-33-7B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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