Method of measuring preload in a multirow bearing assembly

• US 6,460,423 B1
• Filed: 02/01/2001
• Issued: 10/08/2002
• Est. Priority Date: 02/01/2001
• Status: Active Grant

• Current Assignee: The Timken Company
• Original Assignee: The Timken Company
• Inventors: Keller, Larry L., Hasan, Rahil, Harbottle, William E.
• Primary Examiner(s): NOORI, MAX H
• Application Number:
  US09/775,168
• Publication Number:
  US 20020139202A1
• Time in Patent Office: 614 Days
• Field of Search: 738/624.51, 738/624.6, 738/624.71, 738/623.92, 738/624.9
• US Class Current: 73/862.49
• CPC Class Codes: F16C 19/386 in O-arrangement
• CPC Class Codes: F16C 2229/00 Setting preload
• CPC Class Codes: F16C 2326/02 Wheel hubs or castors
• CPC Class Codes: F16C 25/06 Ball or roller bearings
• CPC Class Codes: F16C 33/60 divided or split, e.g. comprising two juxtaposed rings
• CPC Class Codes: F16C 43/04 Assembling rolling-contact bearings
• CPC Class Codes: G01B 7/16 for measuring the deformation in a solid, e.g. by resistance strain gauge

Abstract

The preload in a double row production bearing assembly is ascertained by comparing the deflection produced in that bearing assembly by oppositely directed thrust forces with the deflection produced in a master bearing assembly by equivalent thrust forces likewise applied in opposite directions. The master bearing assembly is similar in configuration and substantially equal in stiffness to the production bearing assembly, but exists in a state of end play. Each thrust force is transferred through the rolling elements of one row and should be sufficient in magnitude to unseat the rolling elements of the other row. The preload in the production bearing assembly equals the end play in the master bearing assembly plus the deflection in the production assembly less the deflection in the master assembly. The endplay in the master bearing assembly is ascertained by extrapolating the deflection to zero thrust force.

Claims

1. A method of ascertaining preload in a first bearing assembly that accommodates rotation about an axis and has at least two rows of rolling elements organized such that the bearing assembly will transfer thrust loads in both axial directions, said method comprising:

applying a single thrust force to the first bearing assembly such that the force is transferred through the assembly in one axial direction, with the force being at a magnitude sufficient to unseat the rolling elements of one of the rows;

applying a single thrust force to the first bearing assembly such that the force is transferred through the bearing assembly in the other axial direction, with that force being of a magnitude sufficient to unseat the rolling elements of the other row;

measuring the deflection that the first bearing assembly undergoes as a consequence of the thrust forces transferred through it; and

comparing the deflection of the first bearing assembly with a known deflection of a second bearing assembly of equivalent stiffness under equivalent thrust forces transferred through the second bearing assembly in both axial directions while the second bearing assembly is set to a condition of known end play.

2. A method according to claim 1 wherein the deflections are compared according to the following formula:

3. The method according to claim 2 wherein thrust forces applied to the first bearing assembly are the same in both axial directions.

4. A method according to claim 1 wherein the first and second bearing assemblies each have inner and outer components between which the rolling elements of those bearing assemblies are located;

and wherein for each bearing assembly one of the components rotates relative to the other component when the forces are transferred through that bearing assembly and the deflection produced by such forces is measured.

5. A method according to claim 4 wherein the deflection for each bearing assembly is measured at multiple locations around the axis for the bearing assembly.

6. A method according to claim 1 wherein the known end play in the second bearing assembly is determined by plotting deflections against thrust forces when multiple thrust loads are transferred through the rolling elements organized to transfer thrust load in one direction;

by plotting deflections against thrust forces when multiple thrust forces are transferred through the rolling elements organized to transfer thrust loads in the opposite direction;

extrapolating to ascertain the deflections when no thrust forces are present; and

determining the dimensional difference between the extrapolated deflections representing zero thrust force.

7. A method according to claim 6 wherein the extrapolation utilizes the least squares fit.

8. A method of ascertaining dimensional preload in a production bearing assembly having an outer component, an inner component, and rolling elements arranged in first and second rows between raceways of the two components, with the rolling elements and raceways for the first row being configured to transfer thrust forces between the inner and outer components in one axial direction and the rolling elements and raceways for the second row being configured to transfer thrust forces between the inner and outer components in the other axial direction, said method comprising:

transferring a thrust force between the two components through the rolling elements of the first row, with the force being of a magnitude sufficient to unseat the rolling elements of the second row;

transferring a thrust force between the two components through the rolling elements of the second row, with the force being of a magnitude sufficient to unseat the rolling elements of the first row;

measuring the deflection of the first component relative to the second component as a consequence the transfer of the thrust forces through both rows of rolling elements; and

comparing the deflection in the production bearing assembly with the deflection in a master bearing assembly of similar configuration and stiffness, but having been set to a condition of known end play, with the deflections being compared at an equivalent thrust force transferred through the first row of rolling elements and another equivalent thrust force transferred through the second row of rolling elements in the master bearing assembly.

9. A method according to claim 8 wherein the deflections of the production and master bearing assemblies are compared according to the following formula:

10. A method according to claim 8 wherein the thrust force applied to the production bearing assembly in the direction which transfers those forces through the first row of rolling elements is the same as the thrust force applied to the production bearing in the direction which transfers the thrust force through the second row of rolling elements.

11. A method according to claim 8 wherein the thrust force which is transferred through the first row of rolling elements in the production assembly is great enough to unseat the rolling elements of the second row from their raceways, and the thrust force which is transferred through the second row of rolling elements in the production assembly is great enough to unseat the rolling elements of the first row from their raceways.

12. A method according to claim 11 wherein the end play in the master bearing assembly is determined by comparing deflections with thrust forces when the thrust loads are transferred through the first rolling elements;

by comparing deflections with thrust forces when multiple thrust forces are transferred through the second row of rolling elements;

extrapolating to ascertain the deflections when no thrust forces are present; and

determining the dimensional difference between the extrapolated deflections representing zero thrust force.

13. A method according to claim 12 wherein the extrapolating utilizes the least squares fit.

14. A method according to claim 8 wherein for each bearing assembly one of the components is rotated relative to the other component about the axis when the thrust forces are transferred through the bearing assembly and the deflection produced is measured.

15. A method according to claim 14 wherein the deflections for each bearing assembly are measured at multiple locations around the axis for that bearing assembly.

16. A method according to claim 8 wherein the inner component of the production bearing assembly is unitary;

wherein the inner component for the master bearing assembly is segmented with the first row of rolling elements for the master bearing assembly being on one segment and the second row being on the another segment.

17. A method according to claim 16 wherein the master bearing assembly includes a spacer that is located between its segments and establishes the known end play of the master bearing assembly.

18. A method according to claim 17 wherein the master bearing assembly is essentially the same as the production bearing assembly, except for the segmented inner component and the spacer.

19. A method of ascertaining dimensional preload in a production bearing assembly having an outer component, an inner component, and rolling elements arranged in first and second rows between raceways on the inner and outer components, with the rolling elements and raceways for the first row being configured to transfer thrust forces between the inner and outer components in one axial direction and the rolling elements and raceways of the second row being configured to transfer thrust forces between the inner and outer components in the other axial direction, said method comprising:

establishing the deflection characteristics of a master bearing that is similar in configuration to the production bearing assembly and has substantially the same stiffness, but differs in that it is set to a condition of end play;

from the deflection characteristics of the master bearing, calculating the end play (Em) in the master bearing assembly;

transferring a first thrust force between the inner and outer components of the master assembly through the rolling elements of the first row;

transferring a second thrust force between the inner and outer components of the master assembly through the rolling elements of the second row;

calculating the deflection (Dm) in the master bearing assembly produced by the first and second thrust forces;

transferring a third thrust force equal to the first thrust force between the inner and outer components of the production assembly through the rolling elements of the first row for the production assembly, transferring a fourth thrust force equal to the second thrust force between the inner and outer components of the production assembly through the rolling elements of the second row for the production assembly;

measuring the deflection Dp produced in the production assembly by the third and fourth thrust forces transferred through its rolling elements; and

calculating the preload in the production bearing assembly according to the following formula;

20. The method according to claim 19 wherein the first thrust force is of a magnitude sufficient to unseat the rolling elements in the second row of the master bearing assembly from their raceways and the second thrust force is of a magnitude sufficient to unseat the rolling elements in the first row of the master bearing assembly from their raceways.

21. The method of claim 20 wherein the deflection characteristics of the master bearing assembly are determined by transferring forces of varying magnitudes between the inner and outer components of the master bearing assembly, with the forces passing through the rolling elements of the first and second rows, and the end play is calculated by extrapolating deflections at low forces to zero force.

22. The method according to claim 21 wherein the deflection characteristics of the master bearing assembly are determined by plotting forces transferred against the deflections caused by such forces.

23. The method according to claim 21 wherein the first and second thrust forces are equal.

24. A method according to claim 19 wherein the inner component of the master bearing assembly is segmented into two segments with the rolling elements of the first row being around the one of the segments and the rolling elements of the second row being around the second element;

and wherein the master bearing assembly also includes a spacer located between the segments to establish the end play in the master bearing assembly.

25. A method of ascertaining preload in a first bearing assembly that accommodates rotation about an axis and has at least two rows of rolling elements organized such that the bearing assembly will transfer thrust loads in both axial directions, said method comprising:

applying a thrust force to the first bearing assembly such that the force is transferred through the assembly in one axial direction;

applying a thrust force to the first bearing assembly such that the force is transferred through the bearing assembly in the other axial direction;

measuring the deflection that the first bearing assembly undergoes as a consequence of the thrust forces transferred through it; and

comparing the deflection of the first bearing assembly with a known deflection of a second bearing assembly under known thrust forces transferred through the second bearing assembly in both axial directions while the second bearing assembly is set to a condition of known end play, with the deflections being compared according to the following formula;

26. A method of ascertaining preload in a first bearing assembly that accommodates rotation about an axis and has at least two rows of rolling elements organized such that the bearing assembly will transfer thrust loads in both axial directions, said method comprising:

applying a thrust force to the first bearing assembly such that the force is transferred through the assembly in one axial direction;

applying a thrust force to the first bearing assembly such that the force is transferred through the bearing assembly in the other axial direction, the forces in both axial directions being the same, the force applied in either direction being transferred through one of the rows of rolling elements and being of a magnitude sufficient to unseat the rolling elements at the other row of rolling elements;

measuring the deflection that the first bearing assembly undergoes as a consequence of the thrust forces transferred through it; and

comparing the deflection of the first bearing assembly with a known deflection of a second bearing assembly under thrust forces that are the same as the thrust forces transferred through the first bearing assembly and are transferred through the second bearing assembly in both axial directions while the second bearing assembly is set to a condition of known end play.

29. The method according to claim 26 wherein the deflections are compared according to the following formula:

27. A method of ascertaining preload in a first bearing assembly that accommodates rotation about an axis and has a unitary inner component, an outer component and at least two rows of rolling elements organized between the inner and outer components such that the bearing assembly will transfer thrust loads in both axial directions, said method comprising:

applying a thrust force to the first bearing assembly such that the force is transferred through the assembly in one axial direction;

applying a thrust force to the first bearing assembly such that the force is transferred through the bearing assembly in the other axial direction;

measuring the deflection that the first bearing assembly undergoes as a consequence of the thrust forces transferred through it; and

comparing the deflection of the first bearing assembly with a known deflection of a second bearing assembly under known thrust forces transferred through the second bearing assembly in both axial directions while the second bearing assembly is set to a condition of known end play, the second bearing assembly being essentially identical in configuration and stiffness to the first bearing assembly with the exception that its inner component is segmented such that one of the rows of rolling elements for the second bearing assembly is around one segment and the other row of rolling elements is around the other segment.

28. A method of ascertaining dimensional preload in a production bearing assembly having an outer component, an inner component, and rolling elements arranged in first and second rows between raceways of the two components, with the rolling elements and raceways for the first row being configured to transfer thrust forces between the inner and outer components in one axial direction and the rolling elements and raceways for the second row being configured to transfer thrust forces between the inner and outer components in the other axial direction, said method comprising:

transferring a thrust force between the two components through the rolling elements of the first row;

transferring a thrust force between the two components through the rolling elements of the second row;

measuring the deflection of the first component relative to the second component as a consequence the transfer of the thrust forces through both rows of rolling elements; and

comparing the deflection in the production bearing assembly with the deflection in a master bearing assembly of similar configuration and stiffness, but having been set to a condition of known end play, with the deflection of the master bearing assembly having been produced by thrust a force transferred through the first row of rolling elements and another thrust force transferred through the second row of rolling elements in the master bearing assembly, the deflections of the production and master bearing assemblies being compared according to the following formula;

30. The method according to claim 28 wherein the thrust forces applied to the production bearing assembly and the thrust forces that were applied to the master bearing assembly are equal.