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Flexible rotor balancing by the influence coefficient method: Multiple critical speeds with rigid or flexible supportsExperimental tests were conducted to demonstrate the ability of the influence coefficient method to achieve precise balance of flexible rotors of virtually any design for operation through virtually any speed range. Various practical aspects of flexible-rotor balancing were investigated. Tests were made on a laboratory quality machine having a 122 cm (48 in.) long rotor weighing 50 kg (110 lb) and covering a speed range up to 18000 rpm. The balancing method was in every instance effective, practical, and economical and permitted safe rotor operation over the full speed range covering four rotor bending critical speeds. Improved correction weight removal methods for rotor balancing were investigated. Material removal from a rotating disk was demonstrated through application of a commercially available laser.
Document ID
19750022493
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tessarzik, J. M.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Publication Information
Publisher: NASA
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-2553
MTI-75TR3
Report Number: NASA-CR-2553
Report Number: MTI-75TR3
Accession Number
75N30566
Funding Number(s)
CONTRACT_GRANT: NAS3-14420
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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