IP Library Granted Patent US 10,183,356
Granted Patent B2
US 10,183,356 · App. 15/812,042 · Granted Jan 22, 2019

Welding tool comprising a shoulder, welding method and workpiece

Inventors: Juergen Silvanus (Munich, DE); Erich Forster (Grossaitingen, DE); Eric Tauscher (Augsburg, DE)
Assignee: Airbus Defence and Space GmbH
B23K20/122B23K20/1245B23K20/1265
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Quick Facts
Patent No.
US 10,183,356
App. No.
15/812,042
Granted
Jan 22, 2019
Kind
B2
Abstract

A welding method for connecting at least two workpieces at a connection region by means of friction stir welding using a welding tool having a probe and a shoulder. The method includes rotating the probe around a rotation axis, wherein the connection region is softened by friction heat provided by the probe during said friction stir welding to form a welded seam at the connection region. The method also includes molding, simultaneously with forming the welded seam, at least one of a bevel, a rounding and a chamfer on an edge of the connection region using the shoulder, wherein the shoulder is configured to separate the connection region from the surroundings.

Claims (11)

1. A welding method for connecting at least two workpieces at a connection region by means of friction stir welding using a welding tool having a probe and a shoulder, the method comprising:

rotating the probe around a rotation axis, wherein the connection region is softened by friction heat provided by the probe during said friction stir welding to form a welded seam at the connection region;

molding, simultaneously with forming the welded seam, at least one of a bevel, a rounding and a chamfer on an edge of the connection region using the shoulder, wherein the shoulder is configured to separate the connection region from the surroundings, and

molding an inner corner of the at least two workpieces onto an inner clamp block.

2. The welding method of claim 1 , further comprising providing a projection on or next to a lateral surface of the shoulder, wherein a projection surface of the projection is arranged on the softened connection region during the friction stir welding process.

3. The welding method of claim 2 , further comprising arranging the projection on a first side of an edge of a first workpiece of the at least two workpieces, and arranging the shoulder on a second side of the edge of the first workpiece.

4. The welding method of claim 2 , further comprising forming a plurality of projections, including the projection, on or next to the shoulder surface.

5. The welding method of claim 2 , wherein the projection surface, together with the lateral surface of the shoulder, has a negative counter-shape to the bevel, the rounding and the chamfer, respectively.

6. The welding method of claim 1 , further comprising non-displaceably fixing the projection on or next to the lateral shoulder surface in a direction of the rotation axis.

7. The welding method of claim 1 , further comprising securing the at least two workpieces against sliding using holder devices during said forming and molding.

8. The welding method of claim 7 , wherein the inner clamp block comprises one of the holder devices.

Assignments (2)
CHANGE OF NAME Recorded Feb 15, 2018
From: EADS DEUTSCHLAND GMBH
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 045348/0858 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 14, 2017
From: SILVANUS, JUERGEN; FORSTER, ERICH; TAUSCHER, ERIC
To: EADS DEUTSCHLAND GMBH
Reel/Frame 044120/0176 →
Priority Claims (1)
DE 10 2011 106 505 · Jun 15, 2011 · national
Continuity (2)
Division 14126335
Related Publication 20180133832A1 · May 17, 2018