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T700 power turbine rotor multiplane/multispeed balancing demonstrationResearch was conducted to demonstrate the ability of influence coefficient based multispeed balancing to control rotor vibration through bending criticals. Rotor dynamic analyses were conducted of the General Electric T700 power turbine rotor. The information was used to generate expected rotor behavior for optimal considerations in designing a balance rig and a balance technique. The rotor was successfully balanced 9500 rpm. Uncontrollable coupling behavior prevented observations through the 16,000 rpm service speed. The balance technique is practical and with additional refinement it can meet production standards.
Document ID
19790017221
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Burgess, G.
(Mechanical Technology, Inc. Latham, NY, United States)
Rio, R.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1979
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-159586
MIT-79-TR-29
Report Number: NASA-CR-159586
Report Number: MIT-79-TR-29
Accession Number
79N25392
Funding Number(s)
CONTRACT_GRANT: NAS3-18520
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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