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Document Number
US Patent 6354741
Issued Date
March 12, 2002
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Abstract
An improved foil thrust bearing includes a pair of members arranged for relative rotation with respect to one another. One of the pair of members is adapted to rotatably support the other. A thrust bearing disk is operatively disposed between the pair of relatively rotatable members. The thrust bearing disk has a plurality of diverging surface ramps. The surface ramps can comprise an inner ramp and an outer ramp. The thrust bearing disk can also comprise a plurality of radial slots. A plurality of separately formed, converging surface compliant foils are disposed on the thrust bearing disk and between the ramps. An underspring element is operatively disposed between the thrust bearing disk and one of the rotatable members, with the underspring element having a plurality of alternating upper and lower ridges.
Drawing
Foil thrust bearing - US Patent 6354741 Drawing
Drawing from US Patent 6354741
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Number of Claims:
18
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Owner
AlliedSignal Inc. (Morristown, NJ)
Published
March 12, 2002
Application Number
09/379,823
Filed
August 24, 1999
US Classification
384/105   384/106 384/124
Int'l Classification
F16C   17/00   (20060101)   F16C   17/12   (20060101)  
Assistant Examiner
Attorney/Law Firm
Parent Case
CROSS REFERENCE TO RELATED APPLICATIONS This application is a continuation-in-part of an application filed on Jan. 22, 1999, Ser. No. 09/235,849. This application also claims the benefit of U.S. Provisional Application filed Feb. 10, 1999, Ser. No. 60/119,581.
USPTO Field of Search
384/103   384/105   384/106   384/124  
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6752533 - Foil thrust bearing cooling - Owned by Honeywell International Inc. (Morristown, NJ)

An improved foil thrust bearing includes a cooling fluid flow turbulence generating disk placed between other foil thrust bearing elements, such as thrust bearing elements and underspring elements. The inventive turbulence generating disk generally provides improved transfer of heat through the foil and into the cooling fluid of foil thrust bearings that may be used for high rotor speed applications. It accomplishes this by improving the transfer of heat through the foil and into the cooling fluid by generating turbulent cooling flow adjacent to the back of the top foil. The turbulent flow is generated primarily by a series of turns or protrusions introduced into the cooling flow stream. Alternate embodiments are disclosed that provide the turbulence generating elements as part of the underside of thrust bearing elements.

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Description
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