IP Library Granted Patent US 10,704,643
Granted Patent B2
US 10,704,643 · App. 16/028,467 · Granted Jul 7, 2020

Damped propshaft assembly and tuned damper for a damped propshaft assembly

Inventors: Jason Ley (Rochester Hills, MI); Zhaohui Sun (Rochester Hills, MI); William Braun (Troy, MI); Jeffrey P. Nyquist (Washington, MI); Michael A. Voight (Troy, MI)
Assignee: American Axle & Manufacturing, Inc.
F16F15/1435B60K17/22F16C3/02F16C3/023F16F15/322B60Y2300/207F16C2204/20F16C2326/06Y10T29/4957Y10T29/49622Y10T29/49904Y10T464/50
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,704,643
App. No.
16/028,467
Granted
Jul 7, 2020
Kind
B2
Abstract

A damped propshaft assembly with a hollow shaft and a tuned damper, which is received in the hollow shaft and includes a liner and a damping member. The liner's mass and stiffness are tuned to attenuate one or more of a bending mode vibration and a torsion mode vibration that occurs at a first predetermined frequency. The liner is not configured to substantially damp shell mode vibration that occurs at a frequency that is not equal to the first predetermined frequency. The damping member is coupled to the liner and is configured to primarily attenuate shell mode vibration in the hollow shaft at one or more desired frequencies. The tuned damper attenuates the at least one of the bending moment vibration and the torsion mode vibration at the first predetermined frequency and also attenuates shell mode vibration. A method for forming a damped propshaft assembly is also provided.

Claims (16)

1. A damped propshaft assembly comprising:

a hollow shaft; and

at least one damper received in the hollow shaft, each of the at least one damper having a structural member, a resilient member and a damping member, the structural member comprising a core, an intermediate member and a cover, the intermediate member being fixedly coupled to the core, the cover being fixedly coupled to the intermediate member and defining a helical gap, the resilient member having a base and a lip member, the base being disposed between the intermediate member and the cover, the lip member being coupled to the base and extending through the helical gap and engaging an interior circumferential surface of the hollow shaft, the damping member being coupled to the cover and engaging the interior circumferential surface of the hollow shaft.

2. The damped propshaft assembly of claim 1 , wherein the damping member is wound onto the cover.

3. The damped propshaft assembly of claim 1 , wherein the damping member provides broadband damping.

4. The damped propshaft assembly of claim 3 , wherein the broadband damping includes damping of shell mode vibration and damping of bending mode vibration at a plurality of frequencies.

5. The damped propshaft assembly of claim 4 , wherein the damping member is a resistive absorber.

6. The damped propshaft of claim 4 , wherein each resilient member of each of the at least one damper is configured to contact the interior circumferential surface of the hollow shaft over a first area, wherein the damping member of each of the at least one damper is configured to contact the interior circumferential surface of the hollow shaft over a second area, and wherein a ratio of first area to the second area is less than or equal to five (5) percent.

7. The damped propshaft assembly of claim 6 , wherein the ratio of the first area to the second area is less than or equal to two and one-half (2.5) percent.

8. The damped propshaft assembly of claim 7 , wherein the ratio of the first area to the second area is less than or equal to one and one-quarter (1.25) percent.

9. The damped propshaft assembly of claim 3 , wherein the broadband damping includes damping of shell mode vibration and damping of torsion mode vibration at a plurality of frequencies.

10. The damped propshaft assembly of claim 9 , wherein the damping member is a resistive absorber.

11. The damped propshaft of claim 9 , wherein each resilient member of each of the at least one damper is configured to contact the interior circumferential surface of the hollow shaft over a first area, wherein the damping member of each of the at least one damper is configured to contact the interior circumferential surface of the hollow shaft over a second area, and wherein a ratio of first area to the second area is less than or equal to five (5) percent.

12. The damped propshaft assembly of claim 11 , wherein the ratio of the first area to the second area is less than or equal to two and one-half (2.5) percent.

13. The damped propshaft assembly of claim 12 , wherein the ratio of the first area to the second area is less than or equal to one and one-quarter (1.25) percent.

14. The damped propshaft assembly of claim 1 , wherein the structural member and the resilient member of each damper form an intermediate damper, and wherein each intermediate damper is not configured to damp shell mode vibration occurring at a frequency that is less than or equal to a predetermined threshold frequency.

Assignments (2)
SECURITY INTEREST Recorded Oct 3, 2025
From: AMERICAN AXLE MANUFACTURING, INC.; MD INVESTORS CORPORATION; AAM NORTH AMERICA, INC.
To: U.S. BANK TRUST COMPANY, NATIONAL ASSOCIATION, AS NOTES COLLATERAL AGENT
Reel/Frame 073005/0001 →
SECURITY INTEREST Recorded May 31, 2022
From: AMERICAN AXLE & MANUFACTURING, INC.
To: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
Reel/Frame 060244/0001 →
Continuity (4)
Continuation 14924940 · Oct 28, 2015
Continuation 14470091 · Aug 27, 2014
Continuation 14254134 · Apr 16, 2014
Related Publication 20180313428A1 · Nov 1, 2018