IP Library Granted Patent US 10,859,117
Granted Patent B2
US 10,859,117 · App. 16/490,346 · Granted Dec 8, 2020

Method of forming a powder metal insert having a horizontal through hole

Inventors: Gary R. Draxler (Slinger, WI); Joel H. Mandel (Hartford, WI)
Assignee: GKN Sinter Metals, LLC
F16C33/145B22D19/00B22F5/10B22F2998/10F16C2360/00
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Quick Facts
Patent No.
US 10,859,117
App. No.
16/490,346
Granted
Dec 8, 2020
Kind
B2
Abstract

A powder metal bearing support insert for casting into an engine component includes a pair of holes formed by interdigitated slots during a powder metal compaction process. Since they are formed by interdigitated slots, this pair of holes may receive the cast material therein during the casting step. Among other things, the cast material in these holes may be drilled or machined using tools graded to work the material of the casting in contrast to the material of the insert.

Claims (19)

1. A powder metal bearing support insert for casting into an engine component, the powder metal bearing support insert comprising:

a body having pair of opposing ends on lateral sides thereof;

a bearing-receiving surface positioned on a side of the body between the pair of opposing ends, the bearing-receiving surface being adapted for reception of a bearing therein;

a pair of holes extending through the body, wherein each of the pair of holes are formed by sets of adjacent interdigitated slots having regions that abut one another to form a connected passageway therethrough that define the respective hole;

wherein the powder metal bearing support insert is formed from a sintered powder metal material such that the powder metal bearing support insert has porosity to accommodate casting the powder metal bearing support insert into an engine component.

2. The powder metal bearing support insert of claim 1 wherein the pair of holes each have a respective central axis and the central axes of the pair of holes are parallel with one another.

3. The powder metal bearing support insert of claim 2 wherein the bearing-receiving surface is semi-cylindrical in shape and has a central axis and wherein the central axis of the bearing-receiving surface is perpendicular to the respective central axes of the pair of holes.

4. The powder metal bearing support insert of claim 1 wherein the respective sets of adjacent interdigitated slots are offset laterally inwardly from each of the pair of opposing ends.

5. The powder metal bearing support insert of claim 4 wherein each of the respective sets of adjacent interdigitated slots create a set of alternating material bridges between a respective one of the pair of opposing ends of the body and a central section of the body in which the central section of the body is disposed between the pair of opposing ends.

6. The powder metal bearing support insert of claim 5 wherein each one of the set of alternating material bridges include a passageway-defining surface that faces a central axis of the passageway and also faces oppositely from an adjacent passageway-defining surface on an adjacent one of the set of alternating material bridges.

7. The powder metal bearing support insert of claim 1 wherein the body is ferrous.

8. An engine component comprising a powder metal bearing insert of claim 1 that is cast into a cast body.

9. The engine component of claim 8 wherein the engine component is one of an engine casing, a cradle, and a bedplate.

10. The engine component of claim 8 wherein the engine component is cast from aluminum or an aluminum alloy and the powder metal bearing support insert is ferrous.

11. The engine component of claim 8 wherein a material of the cast body fills the pair of holes extending through the body of the powder metal bearing support insert.

12. The engine component of claim 11 further comprising holes drilled in the cast body which extend through the pair of holes of the body of the powder metal bearing support insert.

13. A method of casting at least one powder metal bearing support insert of claim 1 into an engine component, the method comprising:

casting the at least one powder metal bearing support insert into the engine component.

14. The method of claim 13 further comprising the step of drilling holes in a cast body of the engine component, the drilled holes extending into the pair of holes of the body of the powder metal bearing support insert.

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 Aug 30, 2019
From: DRAXLER, GARY R.; MANDEL, JOEL H.
To: GKN SINTER METALS, LLC
Reel/Frame 050224/0880 →
Continuity (2)
Provisional Application 62469370 · Mar 9, 2017
Related Publication 20200072280A1 · Mar 5, 2020