System and method for improving a workpiece

Patent metadata

Field	Value
Publication number	US-9541468-B2
Application number	US-201514688091-A
Country	US
Kind code	B2
Filing date	Apr 16, 2015
Priority date	Jan 25, 2013
Publication date	Jan 10, 2017
Grant date	Jan 10, 2017

Abstract

A method of modifying a workpiece includes providing a workpiece, determining a load stress profile associated with a load condition, the load stress profile comprising a load stress greater than a material stress limit of the workpiece, determining a residual stress profile, the residual stress profile comprising a residual stress less than the material stress limit of the workpiece, and providing the workpiece with the residual stress profile, wherein a sum of the load stress and the residual stress is less than the material stress limit of the workpiece.

First claim

What is claimed is:

1. A method of modifying a workpiece, comprising:
providing a workpiece;
determining a tensile load stress profile associated with a tensile load condition;
determining a compressive load stress profile associated with a compressive load condition;
determining a residual stress profile, wherein a sum of the tensile load stress and the residual stress is within a tensile stress limit and a sum of the compressive load stress and the residual stress is within a compressive stress limit of the workpiece; and
providing the workpiece with the residual stress profile.

2. The method of claim 1 , wherein the tensile load stress profile comprises a tensile load stress beyond the tensile stress limit of the workpiece.

3. The method of claim 1 , wherein the compressive load stress profile comprises a compressive load stress within the compressive stress limit of the workpiece.

4. The method of claim 1 , wherein the residual stress profile comprises a residual stress within the tensile stress limit of the workpiece.

5. The method of claim 1 , wherein a magnitude of the sum of the compressive stress and the residual stress is less than a magnitude of a compressive stress limit of the workpiece.

6. The method of claim 1 , wherein the load condition is a cyclic load condition.

7. The method of claim 1 , wherein the workpiece is a gear.

8. The method of claim 1 , wherein providing the workpiece with the residual stress profile comprises performing at least one of a cavitation peening process, a laser peening process, or a low plasticity burnishing process on the workpiece.

9. The method of claim 1 , wherein the determining the compressive load stress profile or determining the tensile load stress profile comprises a finite element analysis of the workpiece.

10. The method of claim 1 , wherein at least one of the compressive load stress profile or the residual stress profile are determined as a function of a depth of the workpiece.

11. The method of claim 1 , wherein at least one of the compressive load stress profile or the residual stress profile are determined as a function of an outer profile translation path of the workpiece.

12. An apparatus comprising:
a processor;
a memory coupled to the processor, wherein the memory comprises instructions that cause the processor to:
determine a tensile limit curve of the workpiece as a function of a dimension of the workpiece;
determine a compressive limit curve of the workpiece as a function of the dimension of the workpiece;
determine a tensile load stress profile associated with a tensile load condition, the tensile load stress profile a function of the dimension of the workpiece;
determine a compressive load stress profile associated with a compressive load condition, the compressive load stress profile a function of the dimension of the workpiece; and
determine a residual stress profile, the residual stress profile a function of the dimension of the workpiece;
wherein a magnitude of a summation of the residual stress profile and the tensile load stress profile is less than a magnitude of the tensile limit curve of the workpiece along the dimension; and
wherein a magnitude of a summation of the residual stress profile and the compressive load stress profile is less than a magnitude of the compressive limit curve along the dimension;

wherein the apparatus is configured to provide the residual stress profile to the workpiece.

13. The apparatus of claim 12 , wherein the dimension is a depth of the workpiece.

14. The apparatus of claim 12 , wherein the dimension is a translational path along an outer surface of the workpiece.

15. An apparatus comprising:
a processor; and
a memory coupled to the processor, wherein the memory comprises instructions that cause the processor to:
determine a first stress associated with a mesh point of a tooth of a gear;
determine a second stress associated with a root of the tooth;
determine a first residual stress to the gear as a function of the first stress; and
determine a second residual stress to the gear as a function of the second stress;
wherein the apparatus is configured to provide at least one of the first residual stress or the second residual stress to the gear.

16. The apparatus of claim 15 , wherein the first stress comprises a bending stress and the second stress comprises a contact stress.

17. The apparatus of claim 15 , wherein a sum of the first stress and the first residual stress is less than a first stress limit of the tooth and wherein a sum of the second stress and the second residual stress is less than a second stress limit of the tooth.

18. The apparatus of claim 15 , wherein a magnitude of a sum of the first stress limit and the first residual stress is less than a magnitude of a first compressive yield limit of the tooth and wherein a magnitude of a sum of the second stress and the second residual stress is less than a magnitude of a second compressive yield limit of the tooth.

19. The apparatus of claim 15 , wherein providing at least one of the first residual stress or providing the second residual stress comprises at least one of laser peening, cavitation peening, or low plasticity burnishing.

20. The apparatus of claim 15 , wherein the first stress and the first residual stress are associated with a first depth associated with the mesh point and wherein the second stress and the second residual stress are associated with a second depth associated with the root.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Ehinger Ryan T
• Woods Ron
• Bockmiller David

Classifications

• B24C1/10

  for compacting surfaces, e.g. shot-peening (for deforming sheet metal, tubes or profiles B21D31/06; as a metallurgical treatment C21D7/00, C22F1/00) · CPC title

• C21D7/02

  by cold working · CPC title

• C21D7/04

  of the surface · CPC title

• G01N3/02

  Details · CPC title

• B23K26/356

  by shock processing · CPC title