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Design of an oil squeeze film damper bearing for a multimass flexible-rotor bearing systemA single-mass flexible-rotor analysis was used to optimize the stiffness and damping of a flexible support for a symmetric five-mass rotor. The flexible, damped support attenuates the amplitudes of motions and forces transmitted to the support bearings when the rotor operates through and above its first bending critical speed. An oil squeeze film damper was designed based on short bearing lubrication theory. The damper design was verified by an unbalance response computer program. Rotor amplitudes were reduced by a factor of 16 and loads reduced by a factor of 36 compared with the same rotor with rigid bearing supports.
Document ID
19750007925
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Cunningham, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Gunter, E. J., Jr.
(Virginia Univ. Cleveland, OH, United States)
Fleming, D. P.
(NASA Lewis Research Center)
Date Acquired
September 3, 2013
Publication Date
February 1, 1975
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TN-D-7892
E-7888
Report Number: NASA-TN-D-7892
Report Number: E-7888
Accession Number
75N15997
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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