TORSIONAL VIBRATION DAMPERS

• US 20160102730A1
• Filed: 10/14/2015
• Published: 04/14/2016
• Est. Priority Date: 10/14/2014
• Status: Active Grant

• Current Assignee: Dayco IP Holdings, LLC (Dayco Products LLC)
• Original Assignee: Dayco IP Holdings, LLC (Dayco Products LLC)
• Inventors: Manzoor, Suhale, Lannutti, Anthony Eugene, Piepsney, William J., Buddington, Christopher R.
• Granted Patent: US 10,151,379 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F16F 15/126 consisting of at least one annular element surrounding the axis of rotation
• CPC Class Codes: F16H 2055/366 with means providing resilience or vibration damping
• CPC Class Codes: F16H 55/36 Pulleys with features essential for adjustment F16H55/52

Abstract

Torsional vibration dampers are disclosed that have a hub having a plate extending radially outward about a shaft-receiving member, a first portion of an inertia member defining a back face and a bore therethrough and having an annular flange concentric about the axis of rotation, a first elastomeric member and a second elastomeric member positioned against opposite sides of the plate, and a second portion of the inertia member fastened to the first portion of the inertia member by one or more fasteners, thereby placing the first and second elastomeric members in compression. The shaft-receiving member of the hub is positioned in the bore with the plate of the hub spaced a distance from an interior surface of the annular flange, and the plate of the hub and the interior surfaces of each of the first and second portions of the inertia member facing the plate define dual common vertices.

Claims

1. A torsional vibration damper comprising:

a hub having a shaft-receiving member defining an axis of rotation and a plate extending radially outward about the shaft-receiving member;

a first portion of an inertia member defining a back face and a bore therethrough and having an annular flange concentric about the axis of rotation, wherein the shaft-receiving member of the hub is positioned in the bore with the plate of the hub spaced a distance from an interior surface of the annular flange;

a first elastomeric member and a second elastomeric member positioned against opposite sides of the plate;

a second portion of the inertia member fastened to the first portion of the inertia member by one or more fasteners thereby placing the first elastomeric member and the second elastomeric member in compression.

2. The torsional vibration damper of claim 1, wherein the one or more fasteners are one or more shoulder bolts connecting the first portion of the inertia member to the second portion of the inertia member with a clearance gap surrounding the fastener through the hub.

3. The torsional vibration damper of claim 1, wherein either of the first portion or the second portion of the inertia member has one or more counterbores and a fastener seated in each counterbore.

4. The torsional vibration damper of claim 1, wherein the hub has minimal parasitic inertia.

5. The torsional vibration damper of claim 1, wherein the annular flange of the inertia member has a belt-engaging surface.

6. The torsional vibration damper of claim 5, wherein the belt engaging surface includes a plurality of grooves.

7. The torsional vibration damper of claim 1, wherein the plate of the hub and the interior surfaces of each of the first and second portions of the inertia member facing the plate define dual common vertices.

8. The torsional vibration damper of claim 7, wherein the opposing surfaces of the plate each define an angled plane of one of the dual common vertices, the interior surfaces of each of the first and second portions of the inertia member facing the plate each define an angled plane of one of the dual common vertices, or both the opposing surfaces of the plate and each of the interior surfaces of the first and second portions of the inertia member facing the plate define angled planes of the dual common vertices.

9. The torsional vibration damper of claim 7, wherein the first and second elastomeric members are spaced a distance apart from the radial inner surface of the annular flange of the first portion of the inertia member.

10. The torsional vibration damper of claim 8, wherein the first elastomeric member comprises concentric O-rings.

20. A system comprising a shaft having the torsional vibration damper of claim 1 mounted thereon with the shaft received in the shaft-receiving member of the hub.

11. A front end accessory drive system comprising:

a torsional vibration damper mounted to a crankshaft, the torsional vibration damper comprising;

a hub having a shaft-receiving member defining an axis of rotation and a plate extending radially outward about the shaft-receiving member;

a first portion of an inertia member defining a back face and a bore therethrough and having an annular flange concentric about the axis of rotation, wherein the shaft-receiving member of the hub is positioned in the bore with the plate of the hub spaced a distance from an interior surface of the annular flange;

a first elastomeric member and a second elastomeric member positioned against opposite sides of the plate;

a second portion of the inertia member fastened to the first portion of the inertia member by one or more fasteners thereby placing the first elastomeric member and the second elastomeric member in compression.

12. The front end accessory drive system of claim 11, wherein the one or more fasteners are one or more shoulder bolts connecting the first portion of the inertia member to the second portion of the inertia member with a clearance gap surrounding the fastener through the hub.

13. The front end accessory drive system of claim 11, wherein the hub has minimal parasitic inertia.

14. The front end accessory drive system of claim 11, wherein the annular flange of the inertia member has a belt-engaging surface.

15. The front end accessory drive system of claim 14, wherein the belt engaging surface includes a plurality of grooves.

16. The front end accessory drive system of claim 11, wherein the plate of the hub and the interior surfaces of each of the first and second portions of the inertia member facing the plate define dual common vertices.

17. The front end accessory drive system of claim 16, wherein the opposing surfaces of the plate each define an angled plane of one of the dual common vertices, the interior surfaces of each of the first and second portions of the inertia member facing the plate each define an angled plane of one of the dual common vertices, or both the opposing surfaces of the plate and each of the interior surfaces of the first and second portions of the inertia member facing the plate define angled planes of the dual common vertices.

18. The front end accessory drive system of claim 16, wherein the first and second elastomeric members are spaced a distance apart from the radial inner surface of the annular flange of the first portion of the inertia member.

19. The front end accessory drive system of claim 17, wherein the first elastomeric member comprises concentric O-rings.