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:
Jun. 04, 2019

Filed:

Jul. 10, 2017
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventor:

Robert Maziarz, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23K 20/12 (2006.01); B23K 20/233 (2006.01); B64C 3/18 (2006.01); B64F 5/00 (2017.01); B23K 101/00 (2006.01); B23K 103/10 (2006.01); B23K 103/18 (2006.01);
U.S. Cl.
CPC ...
B23K 20/122 (2013.01); B23K 20/129 (2013.01); B23K 20/2336 (2013.01); B64C 3/185 (2013.01); B64F 5/00 (2013.01); B23K 2101/006 (2018.08); B23K 2103/10 (2018.08); B23K 2103/18 (2018.08);
Abstract

A method of making an aerospace component such as a spar for an aircraft wing is disclosed. The method includes placing two billets of different alloy in abutting relation, there being no voids or channels formed therebetween, partial penetration friction stir welding together the two billets from opposing sides of the billets, the welds so formed being separated by a central region formed partly by one billet and partly by the other billet, and then machining away material. The machining may be performed so as to leave no portion having a partial penetration friction stir weld, so as to remove all of the central region, and so as to form a multi-alloy spar having at least one transverse web section having a slot formed at least in part by the removal of the central region.


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