Propeller shaft damper with retention lip

US12270448B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12270448-B2
Application numberUS-202217840693-A
CountryUS
Kind codeB2
Filing dateJun 15, 2022
Priority dateJun 15, 2021
Publication dateApr 8, 2025
Grant dateApr 8, 2025

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  1. Title

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  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A propeller shaft assembly includes a propeller shaft extending along an axis between a first and second shaft end. A propeller shaft yoke is operably connected to one of the first or second shaft ends and includes a body presenting a mounting surface extending circumferentially about the axis. A tuned damper extends radially outwardly from the mounting surface and includes a first damper ring disposed in abutting and encircling relationship with the mounting surface and a second damper ring disposed in abutting and encircling relationship with the first damper ring. The tuned damper includes a retention lip extending radially downwardly from the second damper ring in axially spaced relationship with the mounting hub by an axial spacing distance D for protecting the tuned damper from axial impact forces and improving the robustness of the tuned damper mounted on the mounting surface.

First claim

Opening claim text (preview).

What is claimed is: 1. A propeller shaft yoke comprising: a body extending along an axis A from a first yoke end for coupling with a propeller shaft and a second yoke end for coupling with a vehicle driveline component; said body presenting a mounting surface extending circumferentially about said axis A; a tuned damper extending radially outwardly from said mounting surface to define a first damper side disposed adjacent said first yoke end and a second damper side disposed adjacent said second yoke end; said tuned damper including a first damper ring disposed in abutting and encircling relationship with said mounting surface and a second damper ring disposed in abutting and encircling relationship with said first damper ring; and one of said first or second damper sides of said tuned damper including a retention lip extending radially downwardly from said second damper ring and past said first damper ring to a retention lip end disposed in adjacent and axially spaced relationship with said said mounting hub to define an axial spacing distance D between said retention lip and said mounting hub. 2. The propeller shaft yoke as set forth in claim 1 , wherein said retention lip defines a plurality of apertures disposed in circumferentially spaced relationship with one another for establishing an escape path for contaminant build-up in said axial spacing distance D disposed between said retention lip and said mounting hub. 3. The propeller shaft yoke as set forth in claim 2 , wherein each of said plurality of apertures extend radially upwardly from said retention lip end. 4. The propeller shaft assembly as set forth in claim 1 , wherein said retention lip is integrally formed with said second damper ring. 5. The propeller shaft assembly as set forth in claim 1 , wherein said retention lip extends circumferentially about said first damper side of said tuned damper. 6. The propeller shaft assembly as set forth in claim 1 , wherein said retention lip extends circumferentially about said second damper side of said tuned damper. 7. The propeller shaft assembly as set forth in claim 1 , wherein said propeller shaft yoke is comprised of a flange yoke. 8. The propeller shaft assembly as set forth in claim 1 , wherein said propeller shaft yoke is comprised of a slip yoke. 9. The propeller shaft assembly as set forth in claim 1 , wherein said propeller shaft yoke is comprised of a stud yoke. 10. The propeller shaft assembly as set forth in claim 1 , wherein said first damper ring is comprised of a flexible material and said second damper ring is comprised of a steel or iron material. 11. A propeller shaft assembly for connection to a vehicle driveline component, the propeller shaft assembly comprising: a propeller shaft extending along an axis A between a first shaft end and a second shaft end; a propeller shaft yoke operably connected to one of said first or second shaft ends of said propeller shaft; said propeller shaft yoke including a body extending from a first yoke end disposed adjacent said respective first or second shaft end to a second yoke end for coupling with the vehicle driveline component; said body presenting a mounting surface extending circumferentially about said axis; a tuned damper extending radially outwardly from said mounting surface to define a first damper side disposed adjacent said first yoke end and a second damper side disposed adjacent said second yoke end; said tuned damper including a first damper ring disposed in abutting and encircling relationship with said mounting surface and a second damper ring disposed in abutting and encircling relationship with said first damper ring; and one of said first or second damper sides of said tuned damper including a retention lip extending radially downwardly from said second damper ring and past said first damper ring to a retention lip end disposed in adjacent and axially spaced relationship with said mounting hub to define an axial spacing distance D between said retention lip and said mounting hub for protecting said tuned damper from axial impact forces. 12. The propeller shaft assembly as set forth in claim 11 , wherein said retention lip defines a plurality of apertures disposed in circumferentially spaced relationship with one another for establishing an escape path for contaminant build-up in said axial spacing distance D between said retention lip and said mounting hub. 13. The propeller shaft assembly as set forth in claim 12 , wherein each of said plurality of apertures extend radially upwardly from said retention lip end. 14. The propeller shaft assembly as set forth in claim 11 , wherein said retention lip is integrally formed with said second damper ring. 15. The propeller shaft assembly as set forth in claim 11 , wherein said retention lip extends circumferentially about said first damper side of said tuned damper. 16. The propeller shaft assembly as set forth in claim 11 , wherein said retention lip extends circumferentially about said second damper side of said tuned damper. 17. The propeller shaft assembly as set forth in claim 11 , wherein said propeller shaft yoke is comprised of a flange yoke. 18. The propeller shaft assembly as set forth in claim 11 , wherein said propeller shaft yoke is comprised of a slip yoke. 19. The propeller shaft assembly as set forth in claim 11 , wherein said propeller shaft yoke is comprised of a stud yoke. 20. The propeller shaft assembly as set forth in claim 11 , wherein said first damper ring is comprised of a flexible material and said second damper ring is comprised of a steel or iron material.

Assignees

Inventors

Classifications

  • Vibration damping · CPC title

  • the rotating body being a shaft (F16F15/34, F16F15/36 take precedence) · CPC title

  • Shafts; Axles · CPC title

  • Drive shafts · CPC title

  • with, or used as an end stop or buffer; Limiting excessive axial separation · CPC title

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Frequently asked questions

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What does patent US12270448B2 cover?
A propeller shaft assembly includes a propeller shaft extending along an axis between a first and second shaft end. A propeller shaft yoke is operably connected to one of the first or second shaft ends and includes a body presenting a mounting surface extending circumferentially about the axis. A tuned damper extends radially outwardly from the mounting surface and includes a first damper ring …
Who is the assignee on this patent?
Neapco Intellectual Property Holdings Llc
What technology area does this patent fall under?
Primary CPC classification F16F15/1442. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 08 2025 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).