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Flexible rotor balancing by the influence coefficient method. Part 1: Evaluation of the exact point-speed and least squares proceduresThe practical aspects of balancing real, flexible rotors were investigated through inclusion of rotor out-of-roundness data at the measurement probe locations. The computer program was demonstrated to be fully capable of handling out-of-roundness data in the investigation. Testing was performed predominantly with a machine having a 41-inch long, 126-pound rotor. This rotor was operated over a speed range encompassing three rotor-bearing system critical speeds. Both balancing procedures were evaluated for several different conditions of initial rotor unbalance. Safe (and slow) passage through all the critical speeds was obtained after two or three balancing runs in most cases. The Least Squares procedure was found to be generally equivalent in capability to the Exact Point-Speed procedure for the configurations studies. (U)
Document ID
19730005750
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tessarzik, J. M.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1972
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-12107
MTI-72TR32
Report Number: NASA-CR-12107
Report Number: MTI-72TR32
Accession Number
73N14477
Funding Number(s)
CONTRACT_GRANT: NAS3-14420
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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