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Compliant foil fluid film radial bearing

a technology of fluid film bearings and foils, applied in the direction of bearings, shafts and bearings, bearings, etc., can solve the problems of coulomb damping, bearing wear, fluid pressure increase,

Inactive Publication Date: 2006-07-18
CAPSTONE TURBINE
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

"The present invention is about a special bearing that has multiple parts. It includes a bushing, a shaft or rotor, and several layers of flexible foils and springs. The bushing has special retainers that keep it from spinning. These retainers are evenly spaced and run the length of the bushing. They create separate sections where the foils and springs are placed. This design helps to make the bearing work better and last longer."

Problems solved by technology

This results in increases in fluid pressure, especially near the trailing end of the wedge channels.
Flexing and sliding of the foils causes coulomb damping of any axial or overturning motion of the rotating element of the bearing.
This physical contact results in bearing wear.
These preload forces and the high lift-off / touchdown speeds result in significant bearing wear each time the rotor is started or stopped.

Method used

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  • Compliant foil fluid film radial bearing
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Examples

Experimental program
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Embodiment Construction

[0015]Illustrated in FIGS. 1-3 is the compliant foil fluid film radial bearing 10 of the present invention. This multi-segment radial bearing 10 generally comprises a bushing 12, a shaft or rotor 14, a plurality of compliant foils 16 (shown as three), and a like plurality of foil undersprings 18.

[0016]The interior bore 20 of the bushing 12 includes a plurality of anti-rotation devices or retainers 22 (shown as three, generally T-shaped retainers) which are equally spaced and extend the axial length of the interior bore 20. The retainers 22 divide the interior bore 20 of the bushing 12 into a like plurality of lobes 24. The compliant foils 16 and the foil undersprings 18 are disposed in each lobe 24 between adjacent generally T-shaped retainers 22.

[0017]While the shaft or rotor 14 is cylindrical, the interior bore 20 of the bushing 12 may or may not be cylindrical. If the interior bore 20 is not cylindrical, the generally T-shaped retainers 22 will divide the interior bore 20 into a ...

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PUM

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Abstract

A multi-segment radial bearing including a bushing with an interior bore having a plurality of anti-rotation retainers which are equally spaced and extend the axial length of the interior bore. The generally T-shaped retainers divide the interior bore of the bushing into a like plurality of lobes, with each lobe having a compliant foil and a foil underspring disposed between adjacent generally T-shaped retainers.

Description

TECHNICAL FIELD[0001]This invention relates to the general field of compliant foil fluid film bearings and more particularly to an improved multi segment compliant foil fluid film radial bearing.BACKGROUND OF THE INVENTION[0002]Compliant foil fluid film radial bearings are currently being utilized in a variety of high speed rotor applications. These bearings are generally comprised of a bushing, a rotating element such as a rotor or shaft adapted to rotate within the bushing, non-rotating compliant fluid foil members mounted within the bushing and enclosing the rotating element, and non-rotating compliant spring foil members mounted within the bushing underneath the non-rotating compliant fluid foil members. The space between the rotating element and the bushing is filled with fluid (usually air) which envelops the foils. Conventionally, the compliant fluid foil elements are divided into a plurality of individual compliant foils to form a plurality of wedge shaped channels which con...

Claims

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Application Information

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Patent Type & Authority Patents(United States)
IPC IPC(8): F16C17/03F16C17/12F16C27/02
CPCF16C17/024F16C43/02F16C2360/23F16C27/02
Inventor WEISSERT, DENNIS H.
Owner CAPSTONE TURBINE