Bushing for oil film bearing

• US 5,000,584 A
• Filed: 03/02/1990
• Issued: 03/19/1991
• Est. Priority Date: 03/02/1990
• Status: Expired due to Term

• Current Assignee: Morgan Construction Company (Siemens AG)
• Original Assignee: Morgan Construction Company (Siemens AG)
• Inventors: Simmons, Thomas E.
• Primary Examiner(s): Hannon, Thomas R.
• Application Number:
  US07/487,287
• Time in Patent Office: 382 Days
• Field of Search: 384/100, 384/114-118, 384/120, 384/123, 384/283, 384/291, 384/293, 384/322, 384/397
• US Class Current: 384/118
• CPC Class Codes: B21B 31/074 Oil film bearings, e.g. "Morgoil" bearings
• CPC Class Codes: F16C 2322/12 Rolling apparatus, e.g. rolling stands, rolls
• CPC Class Codes: F16C 32/0659 of pockets or grooves
• CPC Class Codes: F16C 33/1075 Wedges, e.g. ramps or lobes, for generating pressure

Abstract

A bushing for an oil film bearing assembly has a plurality of hydrostatic oil recesses in its internal bearing surface at the load zone. Each recess is defined by the intersection of a double curved surface of revolution with the bearing surface, the recess thus being in the form of a portion of a prolate spheroid, with a substantially elliptical feathered peripheral edge.

Claims

1. A bushing for use in an oil film bearing assembly of the type employed to rotatably support the journal surface of a rolling mill roll neck, said bushing comprising:

a wall having an inner cylindrical bearing surface adapted to surround said journal surface;

conduit means extending through said wall for conveying liquid lubricant under pressure to a load zone between said bearing surface and said journal surface; and

at least one recess in said bearing surface in communication with said conduit means for receiving the thus conveyed lubricant under pressure and for distributing the same in said load zone in the form of a lubricant film separating said journal surface from said bearing surface, said recess being defined by the intersection of a double-curved surface of revolution with said bearing surface.

2. The bushing of claim 1 wherein said double-curved surface of revolution is a torus.

3. The bushing of claim 2 wherein the rotational axis of said double-curved surface is parallel to the longitudinal axis of said bushing and surrounded by said bearing surface.

4. The bushing of claim 3 wherein the radius of rotation of said double-curved surface of revolution is smaller than the radius of said bearing surface.

5. The bushing of claim 1 wherein said recess defines a portion of a prolate spheroid.

6. The bushing of claim 1 wherein said recess has a substantially elliptical peripheral edge.

7. The bushing of claim 6 wherein said recess has a major axis extending in a direction perpendicular to the longitudinal bushing axis, and a minor axis extending in a direction parallel to the longitudinal bushing axis.

8. The bushing of claim 7 wherein cross sections taken through said recess in directions perpendicular to said major axis define segments of circles.

9. The bushing of either claim 7 or 8 wherein cross sections taken through said recess in directions perpendicular to said minor axis define portions of circles.

10. A bushing for use in an oil film bearing assembly of the type employed to rotatably support the journal surface of a rolling mill roll neck, said bushing comprising:

a wall having an inner cylindrical bearing surface adapted to surround said journal surface;

conduit means extending through said wall for conveying liquid lubricant under pressure to a load zone between said bearing surface and said journal surface; and

a plurality of recesses in said bearing surface in communication with said conduit means for receiving the thus conveyed lubricant and for distributing the same in said load zone in the form of a lubricant film separating said journal surface from said bearing surface, said recesses being arranged symmetrically with respect to the center of said load zone, each of said recesses having a major axis extending in a direction perpendicular to the longitudinal bushing axis and a minor axis extending in a direction parallel to the longitudinal bushing axis, each of said recesses having a substantially elliptical peripheral edge and a non-uniform depth increasing gradually from said edge to a maximum depth at the intersection of said major and minor axes.