IP Library Granted Patent US 10,494,687
Granted Patent B2
US 10,494,687 · App. 15/546,452 · Granted Dec 3, 2019

Methods and processes of forming gears

Inventor: Bruce D. Hansen (Shelton, CT)
Assignee: SIKORSKY AIRCRAFT CORPORATION
C21D1/06C21D7/06C21D9/32C23C8/20C23C8/22C23C8/80F16H55/06C21D2261/00
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Quick Facts
Patent No.
US 10,494,687
App. No.
15/546,452
Granted
Dec 3, 2019
Kind
B2
Abstract

A method of manufacturing a part is provided. The method includes heating a gear in the presence of carbon to carburize a material of the gear to create a carburized gear, the gear having a plurality of gear teeth and which comprises a selected material. Next, the carburized gear is high pressure gas quenched to drive the carbon into the material of the gear to create a quenched gear. Next, the quenched gear is at least one of cavitation peened and laser peened to create a peened gear. Finally, superfinishing is performed on surfaces of the peened gear.

Claims (13)

1. A method of manufacturing a part, the method comprising:

heating a gear in the presence of carbon to carburize a material of the gear to create a carburized gear, the gear having a plurality of gear teeth and which comprises a selected material;

high pressure gas quenching the carburized gear to drive the carbon into the material of the gear to create a quenched gear;

at least one of cavitation peening and laser peening surfaces of the quenched gear to create a peened gear; and

superfinishing surfaces of the peened gear.

2. The method of claim 1 , wherein the heating and the high pressure gas quenching are performed in a single apparatus without removing the gear from the single apparatus.

3. The method of claim 1 , wherein the at least one of cavitation peening and laser peening generates a layer of induced compressive stresses that is about 0.010 inches (0.025 cm) or thicker.

4. The method of claim 1 , wherein the surfaces of the gear that are subject to the superfinishing are contact surfaces of the plurality of gear teeth.

5. The method of claim 1 , wherein the superfinishing generates a surface roughness between about 1 RA and about 4 RA.

6. The method of claim 1 , wherein the superfinishing generates a surface roughness between about 1 RA and about 2 RA.

7. The method of claim 1 , wherein the carburization hardens the material at about 60 HRC to a depth of about 0.020 inches (0.051 cm) or greater.

8. The method of claim 1 , wherein the carburization hardens the material at about 55 HRC to a depth of between about 0.020 inches (0.051 cm) and about 0.060 inches (0.152 cm).

9. The method of claim 1 , wherein the high pressure gas quenching employs non-reactive gas for quenching.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 16, 2017
From: HANSEN, BRUCE D.
To: SIKORSKY AIRCRAFT CORPORATION
Reel/Frame 043874/0149 →
Continuity (2)
Provisional Application 62111933 · Feb 4, 2015
Related Publication 20180016650A1 · Jan 18, 2018