Deep rolling forming

Patent metadata

Field	Value
Publication number	US-9902482-B2
Application number	US-201514925458-A
Country	US
Kind code	B2
Filing date	Oct 28, 2015
Priority date	Oct 28, 2015
Publication date	Feb 27, 2018
Grant date	Feb 27, 2018

Abstract

Disclosed are a method and system to form a contoured structure using deep rolling. The method includes using deep rolling to introduce plastic deformation to one or more portions of a work piece to form a convex contour in the work piece. The work piece, and subsequently formed contoured structure, can be metal or composite. The disclosed deep rolling systems and methods form, for example contoured aircraft panels, while also providing fatigue strength improvement and low level of work hardening during the forming process rather than as a post-production surface treatment.

First claim

The invention claimed is:

1. A method for forming a contoured structure from a work piece, the method comprising:
providing the work piece comprising a first side and a second side, the work piece having a thickness of about two inches or less;
positioning the work piece on a fixture, such that the first side of the work piece is accessible to a deep rolling tool;
applying a compressive force to the first side of the work piece with the deep rolling tool;
moving the deep rolling tool relative to the work piece while continuing to apply the compressive force to introduce a residual compressive stress localized at or near a surface of the first portion of the work piece;

adjusting the deep rolling tool to contact a second portion of the work piece and moving the deep rolling tool relative to the work piece to introduce a residual compressive stress localized at or near a surface of the second portion of the work piece; and
adjusting the deep rolling tool to contact one or more additional portions of the work piece and moving the deep rolling tool relative to the work piece to introduce a residual compressive stress localized at or near a surface of the one or more additional portions of the work piece and to introduce a convex contour into the work piece, wherein the convex contour has a radius of from one inch to 300 feet.

2. The method of claim 1 , wherein the first portion, second portion, and additional portions of the work piece each comprise a plurality of parallel adjacent line segments.

3. The method of claim 1 , wherein the first portion, second portion, and additional portions of the work piece each comprise a square or rectangular shaped area on the first side of the work piece.

4. The method of claim 1 , wherein the deep rolling tool comprises a spherical ball having a diameter from 0.05 inches to 1 inch or one or more cylinders each cylinder having a dimension of 0.1 inch diameter by 0.25 inches length to 3.0 inches diameter by 12 inches length.

5. The method of claim 1 , wherein an amount of compressive force applied by the deep rolling tool to portions of the work piece range from 0.1 ksi to 30 ksi.

6. The method of claim 1 , wherein moving the deep rolling tool relative to the work piece comprises moving the deep rolling tool at a rate of 0.01 inch/second to 10 inch/second.

7. The method of claim 1 , wherein moving the deep rolling tool relative to the work piece to introduce the residual compressive stress localized at or near the surface of the first, the second, or the one or more additional portions of the work piece comprises moving the deep rolling tool over a same portion of the work piece from 1 to 10 times.

8. The method of claim 1 , wherein a surface roughness of the first side of the contoured structure subsequent to introduction of the residual compressive stress by the deep rolling tool is equal to or less than a surface roughness of the first side of the work piece prior to introduction of the residual compressive stress by the deep rolling tool.

9. The method of claim 1 , wherein the work piece comprises a metal or composite.

10. The method of claim 1 , wherein an amount of force applied by the deep rolling tool to introduce the residual compressive stress to the first portion of the work piece varies.

11. The method of claim 1 , further comprising:
applying another compressive force to the second side of the work piece with a second deep rolling tool to introduce a residual compressive stress localized at or near a surface of a portion of the second side of the work piece.

12. The method of claim 11 , wherein the applying of the another compressive force to the second side of the work piece occurs simultaneously as the compressive force is applied to the first side.

Assignees

• Boeing Co

Inventors

• Zhang Hao
• Quarberg Ryan Paul

Classifications

• B21D31/005

  Incremental shaping or bending, e.g. stepwise moving a shaping tool along the surface of the workpiece (B21D22/14 takes precedence) · CPC title

• B21B1/08

  for rolling {structural sections, i.e.} work of special cross-section, e.g. angle steel (rolling metal of indefinite length in repetitive shapes specially designed for the manufacture of particular objects B21H8/00) · CPC title

• B23P9/02 Primary

  Treating or finishing by applying pressure, e.g. knurling (B23P9/04 takes precedence) · CPC title

• C21D7/08

  by burnishing or the like · CPC title

• B64C1/12 Primary

  Construction or attachment of skin panels · CPC title