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Dual clearance squeeze film damper for high load conditionsSqueeze film dampers are widely used to control vibrations in aircraft turbine engines and other rotating machinery. However, if shaft unbalance rises appreciably above the design value (e.g., due to a turbine blade loss), a conventional squeeze film becomes overloaded, and is no longer effective in controlling vibration amplitudes and bearing forces. A damper concept characterized by two oil films is described. Under normal conditions, only one low-clearance film is active, allowing precise location of the shaft centerline. Under high unbalance conditions, both films are active, controlling shaft vibration in a near-optimum manner, and allowing continued operation until a safe shutdown can be made.
Document ID
19840016996
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fleming, D. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Mechanical Engineering
Report/Patent Number
E-2053
NASA-TM-83619
NAS 1.15:83619
Report Number: E-2053
Report Number: NASA-TM-83619
Report Number: NAS 1.15:83619
Meeting Information
Meeting: Joint Lubrication Conf.
Location: San Diego, CA
Country: United States
Start Date: October 22, 1984
End Date: October 24, 1984
Sponsors: ASME, American Society of Lubrication Engineers
Accession Number
84N25064
Funding Number(s)
PROJECT: RTOP 505-33-5A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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