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Dual clearance squeeze film damperA dual clearance hydrodynamic liquid squeeze film damper for a gas turbine engine is described. Under normal operating conditions, the device functions as a conventional squeeze film damper, using only one of its oil films. When an unbalance reaches abusive levels, as may occur with a blade loss or foreign object damage, a second, larger clearance film becomes active, controlling vibration amplitudes in a near optimum manner until the engine can be safely shut down and repaired.
Document ID
19850025177
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Fleming, D. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
July 9, 1985
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Number: NASA-CASE-LEW-13506-1
Patent Number: US-PATENT-4,527,910
Patent Application Number: US-PATENT-APPL-SN-596960
Accession Number
85N33490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-13506-1|US-PATENT-4,527,910
Patent Application
US-PATENT-APPL-SN-596960
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