IP Library › Granted Patent US 11,219,969
Granted Patent B2
US 11,219,969 · App. 16/774,877 · Granted Jan 11, 2022

Method for the edge-to-edge assembly of two panels using friction stir welding

Inventors: Alain Her (Saint Herbliin, FR); Raphaël Hardy (Orvault, FR)
Assignee: AIRBUS OPERATIONS SAS
B23K26/146B23K20/1265
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Quick Facts
Patent No.
US 11,219,969
App. No.
16/774,877
Granted
Jan 11, 2022
Kind
B2
Abstract

A method for edge-to-edge welding of a first sheet metal panel to a second sheet metal panel on a bearing structure. The method comprises positioning and fixing the first panel to the bearing structure, positioning and fixing the second panel to the bearing structure with the second panel overlapping a raw edge of the first panel, jointly cutting the first panel and the second panel in the overlap area to form a connection edge of the first panel and a connection edge of the second panel, withdrawing scrap cuttings from the first panel and scrap cuttings from the second panel, and friction stir welding the connection edges.

Claims (18)

1. A method for edge-to-edge welding of a first sheet metal panel to a second sheet metal panel, this method comprising:

positioning the first sheet metal panel;

positioning the second sheet metal panel with the second sheet metal panel overlapping a raw edge of the first sheet metal panel to form an overlap area of the first and second sheet metal panels;

jointly cutting the first sheet metal panel and the second sheet metal panel in the overlap area in order to form a connection edge of the first sheet metal panel and a connection edge of the second sheet metal panel;

friction stir welding the connection edges to edge-to-edge weld the first sheet metal panel to the second sheet metal panel;

wherein the cutting step is implemented using a laser cutting method; and

wherein a reflective chute is fitted under the overlap area of the first and second sheet metal panels to form a protection during the laser cutting step.

2. The method according to claim 1 ,

wherein the first sheet metal panel is positioned by being fixed to a bearing structure, and

wherein the second sheet metal panel is positioned by being fixed to this bearing structure.

3. The method according to claim 1 ,

wherein the first sheet metal panel is positioned on a mounting of an apparatus, and

wherein the second sheet metal panel is positioned with respect to the first sheet metal panel by being borne by a handling unit.

4. The method according to claim 1 , wherein the cutting step is implemented using a laser water jet cutting method.

5. The method according to claim 1 , wherein the cutting step produces a cut having a width less than three tenths of a millimeter.

6. The method according to claim 1 , wherein the reflective chute is dimensioned to collect scrap cuttings from the first sheet metal panel at an end of the cutting step.

7. The method according to claim 2 , wherein the bearing structure includes frames, each comprising a notch receiving the reflective chute.

8. The method according to claim 7 , wherein the first and second sheet metal panels are incurved and wherein the frames bearing the first and second sheet metal panels are curved.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2020
From: HARDY, RAPHAËL; HER, ALAIN
To: AIRBUS OPERATIONS SAS
Reel/Frame 051673/0876 →
Priority Claims (1)
FR 1900797 · Jan 29, 2019 · national
Continuity (1)
Related Publication 20200238439A1 · Jul 30, 2020