IP Library Granted Patent US 11,752,550
Granted Patent B2
US 11,752,550 · App. 16/244,406 · Granted Sep 12, 2023

Method for improving fatigue strength on sized aluminum powder metal components

Inventors: Donald Paul Bishop (Stillwater Lake, CA); Matthew D. Harding (Bedford, CA); Richard L. Hexemer, Jr. (Granite Falls, NC); Ian W. Donaldson (Madison, NH)
Assignee: GKN Sinter Metals, LLC
B22F3/24B22F3/14B22F3/16B22F3/162C22C1/0416B22F2003/166B22F2003/247B22F2003/248B22F2201/50B22F2301/052B22F2303/15B22F2998/10C22C21/00C22F1/04
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Quick Facts
Patent No.
US 11,752,550
App. No.
16/244,406
Granted
Sep 12, 2023
Kind
B2
Abstract

A method of manufacturing a sized powder metal component having improved fatigue strength. The method includes the sequential steps of solutionizing a sintered powder metal component and quenching the sintered powder metal component, sizing the sintered powder metal component to form a sized powder metal component, re-solutionizing the sized powder metal component, and ageing the sized powder metal component. The sized powder metal component made by this method, in which the component is re-solutionized between sizing before ageing, can exhibit exceptional improvements in fatigue strength compared to components prepared similarly but that are not re-solutionized.

Claims (25)

1. A method of manufacturing a sized powder metal component having improved fatigue strength over an otherwise identically-processed powder metal component that is not re-solutionized, the method comprising the sequential steps of:

solutionizing a sintered powder metal component comprising an aluminum alloy and quenching the sintered powder metal component;

sizing the sintered powder metal component to form a sized powder metal component;

re-solutionizing the sized powder metal component; and

ageing the sized powder metal component.

2. The method of claim 1 , wherein quenching the sintered powder metal component involves water quenching the sintered powder metal component.

3. The method of claim 1 , wherein quenching the sintered powder metal component involves quenching the sintered powder metal component to ambient temperature.

4. The method of claim 1 , wherein the sized powder metal component has surfaces that are machined.

5. The method of claim 1 , wherein the sized powder metal component has surfaces that are peened.

6. The sized powder metal component made by the method of claim 1 in which the sized powder metal component has improved fatigue strength by virtue of re-solutionizing the sized powder metal component after the step of sizing in comparison to an identical sized powder metal component that has been solutionized, sized, and aged without being additionally re-solutionized after having being sized.

7. The method of claim 1 , wherein, when compared to similar components that were just solutionized and aged according to a T6 treatment, the sized powder metal component subjected to the sequential steps of solutionizing, sizing, re-solutionizing, and ageing have an increase in fatigue strength of between 2.5% and 7.7%.

8. The method of claim 1 , further comprising, before the step of solutionizing the sintered powder metal component, the steps of:

compacting a powder metal to form a powder metal compact; and

sintering the powder metal compact to form the sintered powder metal component.

9. The method of claim 1 , wherein one or both of the steps of solutionizing and re-solutionizing occur at a solutionizing temperature over a solutionizing time during which steps grains of the sintered powder metal component form a homogeneous solid solution.

10. The method of claim 1 , wherein, between the step of solutionizing a sintered powder metal component and quenching the sintered powder metal component and the step of sizing the sintered powder metal component to form a sized powder metal component, the sintered powder metal component is held in air at room temperature for a duration of time.

11. The method of claim 1 , wherein the step of ageing is artificial ageing that occurs at an ageing temperature above ambient temperature over an ageing time.

12. The method of claim 8 , wherein the steps of compacting and sintering occur sequentially.

13. The method of claim 9 , wherein the solutionizing temperature is 530° C. and the solutionizing time is 2 hours.

14. The method of claim 9 , wherein the solutionizing temperature is in a range of 520° C.-540° C.

15. The method of claim 10 , wherein the sintered powder metal component is held in air at room temperature for an hour.

16. The method of claim 11 , wherein the ageing temperature is 190° C. and the ageing time is 12 hours.

17. The method of claim 11 , wherein the ageing temperature is in a range of 180° C. to 200° C.

18. The method of claim 11 , wherein the step of ageing increases the hardness and strength of the sized powder metal component relative to the sized powder metal component prior to the step of ageing.

19. The method of claim 18 , wherein the step of ageing involves ageing to peak hardness.

Assignments (3)
SECURITY INTEREST Recorded Apr 2, 2026
From: AMERICAN AXLE & MANUFACTURING, INC.; GKN SINTER METALS, LLC; GKN DRIVELINE NORTH AMERICA, INC.; GKN DRIVELINE NEWTON, LLC; HOEGANAES CORPORATION
To: JPMORGAN CHASE BANK, N.A.
Reel/Frame 075331/0836 →
SECURITY INTEREST Recorded Apr 1, 2026
From: AMERICAN AXLE & MANUFACTURING, INC.; GKN SINTER METALS, LLC; GKN DRIVELINE NORTH AMERICA, INC.; GKN DRIVELINE NEWTON, LLC; HOEGANAES CORPORATION
To: U.S. BANK TRUST COMPANY, NATIONAL ASSOCIATION,, AS NOTES COLLATERAL AGENT
Reel/Frame 075325/0112 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 10, 2019
From: BISHOP, DONALD P.; HARDING, MATTHEW D.; HEXEMER, RICHARD L., JR.; DONALDSON, IAN W.
To: GKN SINTER METALS, LLC
Reel/Frame 047953/0351 →
Continuity (2)
Provisional Application 62615799 · Jan 10, 2018
Related Publication 20190210112A1 · Jul 11, 2019