The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 24, 2016

Filed:

Feb. 27, 2015
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Domenico Furfari, Hamburg, DE;

Marco Pacchione, Hamburg, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23K 20/12 (2006.01); B23K 31/02 (2006.01); B23K 37/08 (2006.01); B23K 20/00 (2006.01); B23K 20/26 (2006.01);
U.S. Cl.
CPC ...
B23K 20/129 (2013.01); B23K 20/002 (2013.01); B23K 20/122 (2013.01); B23K 20/123 (2013.01); B23K 20/124 (2013.01); B23K 20/126 (2013.01); B23K 20/1245 (2013.01); B23K 20/1275 (2013.01); B23K 20/26 (2013.01); B23K 31/02 (2013.01); B23K 37/08 (2013.01);
Abstract

A method for the friction stir welding of two components, in particular of two shell components of a fuselage structure of an aircraft and spacecraft, said method comprising the following method steps: positioning the two components relative to one another in such a way that a connection region is formed between the two components; friction stir welding the two components by means of a friction stir welding tool which penetrates the connection region in order to produce a weld which permeates the connection region with the formation of an unpenetrated weld edge portion of the connection region; and introducing internal compressive stresses, at least in the weld edge portion of the connection region. Further a device for the friction stir welding of two components, in particular of two shell components of a fuselage structure of an aircraft and spacecraft is provided.


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