Roto peening orbital drilling tool

Patent metadata

Field	Value
Publication number	US-10434624-B2
Application number	US-201615204226-A
Country	US
Kind code	B2
Filing date	Jul 7, 2016
Priority date	Jul 7, 2016
Publication date	Oct 8, 2019
Grant date	Oct 8, 2019

Abstract

A machining tool incorporates a shaft having a first end configured to fit into a machining collet. A cutting portion extends from a second end of the shaft. A residual stress inducer is located between the first and second ends and includes a torsion element joined to the shaft at a connection end. A carbide tip is present on a free end opposite the connection end and the torsion element is configured such that a selected rotational speed, altered from a normal cutting speed, causes the carbide tip of the torsion element to contact a workpiece surface.

First claim

What is claimed is:

1. A machining tool comprising:
a shaft having a first end configured to fit into a machining collet;
a cutting portion extending from a second end of the shaft;
a residual stress inducer located between the first and second ends, the residual stress inducer having:
a torsion element having a connection end and a free end, said torsion element joined to the shaft at the connection end;
a carbide tip on the free end of the torsion element opposite the connection end,
the torsion element configured such that at a selected rotational speed, altered from a cutting speed, the carbide tip of the torsion element contacts a workpiece surface.

2. The machining tool as defined in claim 1 wherein the carbide tip comprises a plurality of carbide balls.

3. The machining tool as defined in claim 2 further comprising a flexible element intermediate the carbon balls and a body of the torsion element.

4. The machining tool as defined in claim 3 wherein the flexible element comprises a fabric flap.

5. The machining tool as defined in claim 1 further comprising a rotational element connecting the connection end of the torsional element to the shaft.

6. The machining tool as defined in claim 5 wherein the rotational element comprises a hinge.

7. The machining tool as defined in claim 5 wherein the rotational element comprises a rotary spring.

8. The machining tool as defined in claim 1 further comprising a spring providing centripetal force urging a body portion of the torsion element toward the shaft.

9. The machining tool as defined in claim 1 wherein the residual stress inducer comprises a first peening element and a second peening element and further comprising a spring interconnecting the torsion element of the first peening element through the shaft to the torsion element of the second peening element.

10. The machining tool as defined in claim 9 further comprising a slot in the shaft receiving the spring.

11. A method for inducing residual stress in a workpiece surface comprising:
machining the work piece at a cutting speed with a machine tool having
a shaft having a first end configured to fit into a machining collet,
a cutting portion extending from a second end of the shaft,
a residual stress inducer located between the first and second ends, the residual stress inducer having:
a torsion element having a connection end and a free end, said torsion element joined to the shaft at the connection end;
a carbide tip on the free end of the torsion element opposite the connection end,
the torsion element configured such that at a selected rotational speed, altered from a cutting speed, the carbide tip of the torsion element contacts a workpiece surface;

resiliently restraining the residual stress inducer within an outer diameter of the cutting portion at the cutting speed; and,
altering rotational speed of the tool to a selected rotational speed thereby extending the torsion element causing contact with the workpiece surface by the carbide tip on the torsion element.

12. The method as defined in claim 11 wherein the step of altering the rotational speed comprises increasing to a second speed to increase centrifugal force on the torsion element.

13. The method as defined in claim 12 wherein the step of altering the rotational speed comprises reversing direction of the rotation and rotating at an extension speed.

14. The method as defined in claim 12 further comprising employing aerodynamic force on the torsion element to assist in expanding the torsional element into contact with the surface of the workpiece.

15. The method as defined in claim 12 further comprising reducing the rotational speed of the tool to retract the torsion elements.

Assignees

• Boeing Co

Inventors

• Farrell Nicholas R
• Gamboa James D
• Holleman Wesley E
• Lipczynski Gary

Classifications

• B23C2270/04

  Use of centrifugal force · CPC title

• B23P9/00

  Treating or finishing surfaces mechanically, with or without calibrating, primarily to resist wear or impact, e.g. smoothing or roughening turbine blades or bearings (treatment covered by a single other subclass, see the relevant subclass, e.g. B24C, C21D7/00, C22F1/00); Features of such surfaces not otherwise provided for, their treatment being unspecified · CPC title

• B23B51/08

  Drills combined with tool parts or tools for performing additional working {(B23G5/20 takes precedence)} · CPC title

• B23C5/10

  Shank-type cutters, i.e. with an integral shaft · CPC title

• B23C2220/605

  Roughing and finishing · CPC title