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T55 power turbine rotor multiplane-multispeed balancing studyA rotordynamic analysis of the T55-L-11C engine was used to evaluate the balancing needs of the power turbine and to optimize the balancing procedure. As a result, recommendations were made for implementation of a multiplane-multispeed balancing plan. Precision collars for the attachment of trial weights to a slender rotor were designed enabling demonstration balancing on production hardware. The quality of the balance was then evaluated by installing a high speed balanced power turbine in an engine and running in a test cell at the Corpus Christi Army depot. The engine used had been tested prior to the turbine changeout and showed acceptable overall vibration levels for the engine were significantly reduced, demonstrating the ability of multiplane-multispeed balancing to control engine vibration.
Document ID
19830025623
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Martin, M. R.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
MTI-83TR55
NAS 1.26:167891
NASA-CR-167891
Report Number: MTI-83TR55
Report Number: NAS 1.26:167891
Report Number: NASA-CR-167891
Accession Number
83N33894
Funding Number(s)
CONTRACT_GRANT: NAS3-19408
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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