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The Chevron Foil Thrust Bearing: Improved Performance Through Passive Thermal Management and Effective Lubricant MixingAn improved foil thrust bearing is described that eliminates or reduces the need for forced cooling of the bearing foils while at the same time improves the load capacity of the bearing, enhances damping, provides overload tolerance, and eliminates the high speed load capacity drop-off that plagues the current state of the art. The performance improvement demonstrated by the chevron foil thrust bearing stems from a novel trailing edge shape that splays the hot lubricant in the thin film radially, thus preventing hot lubricant carry-over into the ensuing bearing sector. Additionally, the chevron shaped trailing edge induces vortical mixing of the hot lubricant with the gas that is naturally resident within the inter-pad region of a foil thrust bearing. The elimination of hot gas carry-over in combination with the enhanced mixing has enabled a completely passive thermally managed foil bearing design. Laboratory testing at NASA has confirmed the original analysis and reduced this concept to practice.
Document ID
20140010151
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Bruckner, Robert
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
July 24, 2014
Publication Date
September 8, 2013
Subject Category
Aircraft Propulsion And Power
Mechanical Engineering
Report/Patent Number
GRC-E-DAA-TN8502
Meeting Information
Meeting: World Tribology Congress
Location: Torino, Italy
Country: Italy
Start Date: September 8, 2013
End Date: September 13, 2013
Sponsors: Italian Tribology Association
Funding Number(s)
WBS: WBS 016541.01.03.A061.13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
foil bearing
gas bearing
thrust bearing
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