Manufacturing process for aerospace bearing rolling elements

Patent metadata

Field	Value
Publication number	US-9732394-B2
Application number	US-201213474407-A
Country	US
Kind code	B2
Filing date	May 17, 2012
Priority date	May 17, 2012
Publication date	Aug 15, 2017
Grant date	Aug 15, 2017

Abstract

A method of treating bearing rolling elements or bearing rings after a hardening and temper heat treatment is disclosed. The method may include treating the bearing rolling elements in a tumbling treatment and then in a duplex hardening treatment. The method may include treating the bearing rings in a peening treatment and then in a duplex hardening treatment. The duplex hardening treatment may also include at least one sequential process segment consisting of subjecting the bearing rolling element & rings to a nitriding process to increase the surface hardness and compressive residual stress. The combined two-step process produces a deep surface/sub-surface residual stress greater than the depth of the maximum operating von-Mises shear stress along with an ultra-hard surface with high magnitude of compressive residual stress. In so doing, the bearing ring and rolling elements will have significantly enhanced rolling contact fatigue resistance and resistance to surface imperfections and debris.

First claim

What is claimed is:

1. A method of treating bearing components after a heat treatment, the method comprising:
performing a tumbling treatment of bearing rolling elements to induce a first surface/sub-surface compressive residual stress into the bearing rolling element at a first depth; and
applying duplex hardening treatment after the tumbling treatment to induce a second surface compressive residual stress into the bearing rolling element;
wherein the duplex hardening treatment introduces the second surface compressive residual stress to a second depth different than the first depth and of no more than about 0.004 inch.

2. The method of claim 1 , wherein the tumbling treatment comprises:
placing the bearing rolling elements in barrels on a tumbling machine; and
operating the tumbling machine for a time sufficient to induce the first surface/sub-surface compressive residual stress profile.

3. The method of claim 2 , wherein the tumbling treatment comprises producing a plastically deformed surface/sub-surface region with the first surface/subsurface compressive residual stress to a first depth greater than a depth of a design maximum von-Mises shear stress.

4. The method of claim 3 , wherein the first depth is at least about 0.020 inch.

5. The method of claim 1 , wherein the bearing rolling element is made of a high strength, low or medium alloy martensitic steel comprising AISI 52100 and AISI M50.

6. The method of claim 1 , wherein a tumbling media is placed with the bearing rolling elements in the barrels on the tumbling machine.

7. The method of claim 1 , wherein the duplex hardening treatment
comprises:
subjecting the bearing rolling element to at least one sequential process segment to induce the first surface compressive residual stress, wherein the process segment consists of subjecting the bearing rolling element to a boost period in an atmosphere containing active nitrogen, and then subjecting the bearing rolling element to a diffuse period in an atmosphere free of active nitrogen.

8. The method of claim 7 , wherein a total process time during all boost and diffuse periods is about 40 to 80 hours, comprising boost periods of about 2 to 20 hours each, and diffuse periods of about 2 to 60 hours each, wherein a temperature is maintained between about 400° C. and about 600° C. during both the boost and diffuse periods, and wherein an amount of active nitrogen used during each boost periods may be the same or varied.

9. The method of claim 1 , wherein the second depth is in the range from about 0.0008 inch to about 0.0036 inch.

10. The method of claim 1 , wherein the bearing rolling element has an improved rolling contact fatigue/endurance limit life.

11. The method of claim 1 , wherein the bearing rolling element forms a surface having increased hardness compared to an untreated surface, and has a compressive surface residual stress greater than the untreated surface.

Assignees

• Chin Herbert A
• Ogden William P
• Haluck David A
• Mccutchan Sean
• Spitzer Ronald F
• Keller Allen V
• United Technologies Corp

Inventors

• Chin Herbert A
• Ogden William P
• Haluck David A
• Mccutchan Sean
• Spitzer Ronald F
• Keller Allen V

Classifications

• B24B31/02

  involving rotary barrels · CPC title

• C23C8/80

  After-treatment · CPC title

• Y10T29/47

  Burnishing · CPC title

• F16C2360/23

  Gas turbine engines · CPC title

• F16C2223/02

  Mechanical treatment, e.g. finishing · CPC title