IP Library Granted Patent US 11,898,608
Granted Patent B2
US 11,898,608 · App. 15/954,703 · Granted Feb 13, 2024

Tolerance ring, method, and assembly for component retention control

Inventors: Florian Itta (Renchen, DE); Charles Gage (Bristol, GB); Stephen Saunders (Bristol, GB)
Assignee: SAINT-GOBAIN PERFORMANCE PLASTICS RENCOL LIMITED
F16D1/0835F16D7/021Y10T403/7061
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Quick Facts
Patent No.
US 11,898,608
App. No.
15/954,703
Granted
Feb 13, 2024
Kind
B2
Abstract

A tolerance ring including a sidewall and at least one projection from the sidewall that projects radially and axially to prevent axial displacement of the tolerance ring with respect to a component interior or exterior to the tolerance ring.

Claims (30)

1. A tolerance ring configured to be mounted between an inner shaft component and an outer housing component, comprising:

an annular sidewall comprising at least one bore extending therethrough, wherein each bore is disposed axially inward from a first axial edge of the sidewall; and

at least one projection extending radially and axially from the sidewall configured to abut an axial end surface of the inner shaft component or the outer housing component to prevent axial displacement of the tolerance ring, with respect to the inner component or the outer component, each projection comprising a pair of circumferentially-spaced radial flaps located on opposing axially-extending edges of a respective one of the bores, wherein both radial flaps are bent inwardly and outwardly in the same radial direction from the sidewall, and wherein each flap extends radially inward from perspective edge of he bore along a first side of the flap and is continuously disconnected from the bore along the remaining sides of the flap such that an end portion of each flap axially fills a portion of the bore; and

a plurality of circumferentially-spaced axially-extending wave structures protruding radially from the sidewall adjacent a second axial edge thereof configured to engage an outer surface of the inner shfat component or an inner surface of the outer housing component, wherein an unformed section of the sidewall is located between each pair of adjacent wave structures, and wherein the radial flaps and the wave structures extend in the same radial direction from the sidewall.

2. The tolerance ring of claim 1 , wherein each wave structure extends radially outward from the sidewall.

3. The tolerance ring of claim 1 , wherein each wave structure extends radially inward from the sidewall.

4. The tolerance ring of claim 1 , wherein the flaps have a radial height H P that is greater than a radial height H W of at least one of the wave structures. Add Go for FIG. 10 embodiment.

5. The tolerance ring of claim 1 , wherein the tolerance ring further comprises an axial gap in the sidewall.

6. The tolerance ring of claim 1 , wherein each projection extends radially outward from the sidewall.

7. The tolerance ring of claim 1 , wherein each projection extends radially inward from the sidewall.

8. The tolerance ring of claim 1 , wherein the tolerance ring comprises a substrate and a low friction material overlying the substrate.

9. The tolerance ring of claim 8 , wherein the low friction material comprises a polymer.

10. An assembly, comprising:

an outer housing component;

an inner shaft component; and

a tolerance ring mounted between the inner shaft component and the outer housing component, the tolerance ring comprising:

an annular sidewall comprising at least one bore extending therethrough, wherein each bore is disposed axially inward from a first axial edge of the sidewall; and

at least one projection extending radially and axially from the sidewall configured to abut an axial end surface of the inner shaft component or the outer housing component to prevent axial displacement of the tolerance ring, with respect to the inner component or the outer component, each projection comprising a pair of circumferentially-spaced radial flaps located on opposing axially-extending edges of a respective one of the bores, wherein both radial flaps are bent inwardly and outwardly in the same radial direction from the sidewall, and wherein each flap extends radially inward from perspective edge of he bore along a first side of the flap and is continuously disconnected from the bore along the remaining sides of the flap such that an end portion of each flap axially fills a portion of the bore; and

a plurality of circumferentially-spaced axially-extending wave structures protruding radially from the sidewall adjacent a second axial edge thereof configured to engage an outer surface of the inner shfat component or an inner surface of the outer housing component, wherein an unformed section of the sidewall is located between each pair of adjacent wave structures, and wherein the radial flaps and the wave structures extend in the same radial direction from the sidewall.

11. The assembly of claim 10 , wherein the inner component comprises a rolling-element bearing assembly.

12. The assembly of claim 10 , wherein the tolerance ring is fixed to the outer or inner component by any of the following processes: form fit, force fit, bonding.

13. The assembly of claim 10 , wherein the outer or inner component includes a groove.

14. The assembly of claim 10 , wherein the outer or inner component contains at least one projection or depression.

15. A method, comprising:

providing an inner shaft component and an outer housing component;

positioning a tolerance ring between the inner shaft component and the outer housing component, the tolerance ring comprising:

an annular sidewall comprising at least one bore extending therethrough, wherein each bore is disposed axially inward from a first axial edge of the sidewall; and

at least one projection extending radially and axially from the sidewall configured to abut an axial end surface of the inner shaft component or the outer housing component to prevent axial displacement of the tolerance ring, with respect to the inner component or the outer component, each projection comprising a pair of circumferentially-spaced radial flaps located on opposing axially-extending edges of a respective one of the bores, wherein both radial flaps are bent inwardly and outwardly in the same radial direction from the sidewall, and wherein each flap extends radially inward from perspective edge of he bore along a first side of the flap and is continuously disconnected from the bore along the remaining sides of the flap such that an end portion of each flap axially fills a portion of the bore; and

a plurality of circumferentially-spaced axially-extending wave structures protruding radially from the sidewall adjacent a second axial edge thereof configured to engage an outer surface of the inner shfat component or an inner surface of the outer housing component, wherein an unformed section of the sidewall is located between each pair of adjacent wave structures, and wherein the radial flaps and the wave structures extend in the same radial direction from the sidewall; and

contacting the projection to one of the inner shaft component or the outer housing component to retain the tolerance ring to the inner component or the outer component.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 9, 2018
From: ITTA, FLORIAN; GAGE, CHARLES; SAUNDERS, STEPHEN
To: SAINT-GOBAIN PERFORMANCE PLASTICS RENCOL LIMITED
Reel/Frame 046297/0954 →
Continuity (2)
Provisional Application 62488394 · Apr 21, 2017
Related Publication 20180306248A1 · Oct 25, 2018
Cited By (5)
US 1,062,635 US 1,065,994 US 12,519,294 US 12,553,343 US 12,674,315