IP Library Granted Patent US 7,485,044
Granted Patent B2
US 7,485,044 · App. 11/059,820 · Granted Feb 3, 2009

Shaft assembly and method of manufacture thereof

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Quick Facts
Patent No.
US 7,485,044
App. No.
11/059,820
Granted
Feb 3, 2009
Kind
B2
Abstract

A shaft assembly comprises an annular hub with a shaft extending therefrom. The hub and the shaft are integrally formed from a single forging, thereby reducing stress concentration locations within the assembly. The hub includes a circumferential wall having a wall thickness. A plurality of teeth protrude from the circumferential wall. Each of the plurality of teeth has a tooth thickness, with the tooth thickness being greater than the wall thickness. Splines are formed on an outer surface of the shaft. Preferably, the splines are induction hardened. A method of manufacturing the shaft assembly includes forging a base member and flow forming the base member into the hub and the shaft to create the shaft assembly. Next, the plurality of teeth are formed within the hub. Finally, the splines are formed on the shaft, and preferably induction hardened.

Claims (34)

1. A shaft assembly comprising:

an annular hub including a circumferential wall having a wall thickness;

wherein said circumferential wall is cylindrical;

a shaft extending from said hub, said hub and said shaft being integrally formed from a single forging, thereby eliminating stress concentration locations;

wherein said shaft is hollow from said hub to an end of said shaft opposite said hub;

a plurality of teeth integrally formed with said circumferential wall and protruding from said circumferential wall, with each of said plurality of teeth having a tooth thickness, said tooth thickness being greater than said wall thickness;

wherein each of said plurality of teeth is solid;

induction hardened splines formed on an outer surface of said shaft; and

wherein said plurality of teeth and said induction hardened splines are formed after said single forging.

2. The shaft assembly of claim 1 , wherein said splines are induction hardened to a Rockwell hardness of between 50 and 55.

3. The shaft assembly of claim 1 , wherein said splines are formed at the end of said shaft opposite said hub.

4. The shaft assembly of claim 1 , wherein said plurality of teeth are distributed about the periphery of said circumferential wall.

5. The shaft assembly of claim 1 , wherein said tooth thickness is at least twice said wall thickness; and wherein said tooth thickness for each of said plurality of teeth is a distance between said circumferential wall and an outer surface of said each of said plurality of teeth.

6. The shaft assembly of claim 1 , wherein said circumferential wall includes a first edge and a second edge, and wherein each of said plurality of teeth extends from said first edge to said second edge.

7. The shaft assembly of claim 1 , wherein at least one of said plurality of teeth includes an opening through said at least one of said plurality of teeth and said circumferential wall into said annular hub, to allow lubricant into and out of said shaft assembly; and wherein said opening is formed after said single forging.

8. The shaft assembly of claim 1 , wherein said hub and said shaft comprise steel having a Rockwell hardness of between 65 and 70.

9. A shaft assembly comprising:

an annular hub including a circumferential wall defining first and second edges, said circumferential wall having a wall thickness;

wherein said circumferential wall is cylindrical;

a plurality of teeth integrally formed with said circumferential wall and protruding about the entire periphery of said circumferential wall and extending between said first and second edges, with each of said plurality of teeth having a tooth thickness, said tooth thickness being greater than said wall thickness;

a shaft extending from said hub to a spline end, said hub and said shaft being flow formed from a single forging, thereby eliminating stress concentration locations;

wherein said shaft is hollow from said hub to said spline end;

splines formed on an outer surface of said shaft at said spline end, said splines being induction hardened to a Rockwell hardness of between 50 and 55; and

wherein said plurality of teeth and said induction hardened splines are formed after said single forging.

10. A shaft assembly comprising:

an annular hub including a circumferential wall having a wall thickness;

wherein said circumferential wall is cylindrical;

wherein said annular hub mates with a clutch;

a plurality of teeth integrally formed with said circumferential wall and protruding from said circumferential wall, with each of said plurality of teeth having a tooth thickness, said tooth thickness being greater than said wall thickness;

a shaft extending from said hub and configured to support a gear, said hub and said shaft being integrally formed from a single forging, thereby eliminating stress concentration locations;

wherein said shaft is hollow from said hub to an end of said shaft opposite said hub;

induction hardened splines formed on an outer surface of said shaft; and

wherein said plurality of teeth and said induction hardened splines are formed after said single forging.

11. The shaft assembly of claim 10 , wherein each of said plurality of teeth is solid.

Assignments (13)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034371/0676 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025780/0936 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025327/0001 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025245/0442 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025311/0770 →
SECURITY AGREEMENT Recorded Aug 28, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023162/0001 →
SECURITY AGREEMENT Recorded Aug 27, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023156/0052 →
RELEASE OF SECURITY INTEREST Recorded Aug 21, 2009
From: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023127/0468 →
RELEASE OF SECURITY INTEREST Recorded Aug 20, 2009
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023124/0429 →
SECURITY AGREEMENT Recorded Apr 16, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
Reel/Frame 022553/0446 →
SECURITY AGREEMENT Recorded Feb 4, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 022201/0610 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 14, 2009
From: GENERAL MOTORS CORPORATION
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 022117/0022 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 7, 2005
From: BRIGGS, ROGER L.
To: GENERAL MOTORS CORPORATION
Reel/Frame 016024/0326 →