IP Library Granted Patent US 9,815,152
Granted Patent B2
US 9,815,152 · App. 15/051,374 · Granted Nov 14, 2017

Friction stir welding: method and device for filling a hole at the end of welding or for repairing a welding defect

Inventors: Gilles Foucher (Chatillon sous Bagneux, FR); François Marie (Rueil Malmaison, FR); Daniel Aliaga (Bron, FR)
Assignee: AIRBUS
B23P6/04B23K20/124B23K20/128B23K20/1265B23K20/22B23P6/00
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Quick Facts
Patent No.
US 9,815,152
App. No.
15/051,374
Granted
Nov 14, 2017
Kind
B2
Abstract

A method for repairing a defect affecting a weld. A sheet of filler metal is placed on the surface of the welded part, next to the region of the defect. The sheet is locally welded to the welded part in the region of the defect using a friction stir welding tool having a retractable welding pin. The welded part and the sheet are separated such that the filler metal amalgamated with the metal of the welded part remains in position. The local welding operation includes successively performing the following: setting the welding tool into rotation and putting it under pressure; inserting the pin to a small distance from the anvil while maintaining or increasing the pressure on the shoulder of the welding tool; progressively retracting the pin while maintaining or increasing the pressure on the shoulder; and stopping the pressure on the shoulder when the retractable pin has been retracted.

Claims (13)

1. A method for reworking a defect affecting a weld, comprising the steps of:

placing a sheet of a filler metal in a region of the defect, the sheet of the filler metal being placed on a surface of a welded part next to the region of the defect;

locally welding the sheet of the filler metal to the welded part, the welding being carried out in the region of the defect with the aid of a friction stir welding tool comprising a retractable welding pin; and

separating the welded part and the sheet of the filler metal to leave the filler metal in place in a manner amalgamated by welding with a metal of the welded part;

wherein the step of separating is performed at the end of the locally welding step, by imparting a movement on the sheet of the filler metal in a plane of the welded part before a rotation of the friction stir welding tool stops.

2. The method according to claim 1 , wherein the step of locally welding comprises the following successive steps of:

setting the friction stir welding tool into rotation and putting the friction stir welding tool under a pressure;

inserting the retractable welding pin progressively into the welded part while maintaining or increasing the pressure on a shoulder of the friction stir welding tool;

progressively retracting the retractable welding pin while maintaining or increasing the pressure on the shoulder of the friction stir welding tool;

stopping the pressure on the shoulder of the friction stir welding tool upon withdrawal of the retractable welding pin from a top of the welded part.

3. The method according to claim 2 , wherein the step of inserting the retractable welding pin is accompanied by the step of inserting the shoulder of the friction stir welding tool at a movement rate slower than that of the retractable welding pin.

4. The method according to claim 2 , wherein the step of inserting the retractable welding pin is accompanied by a continuous orbital movement of the retractable welding pin.

5. The method according to claim 1 , further comprising the step of renewing a surface state of the welded part in the region of the defect.

Assignments (2)
MERGER Recorded Oct 9, 2017
From: AIRBUS GROUP SAS
To: AIRBUS
Reel/Frame 043816/0916 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 1, 2016
From: FOUCHER, GILLES; MARIE, FRANÇOIS; ALIAGA, DANIEL
To: AIRBUS GROUP SAS
Reel/Frame 037972/0021 →
Priority Claims (1)
EP 15156759 · Feb 26, 2015 · regional
Continuity (1)
Related Publication 20160250727A1 · Sep 1, 2016