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. 26, 2020

Filed:

Feb. 24, 2017
Applicant:

Spirit Aerosystems, Inc., Wichita, KS (US);

Inventor:

Heath Edward Misak, Wichita, KS (US);

Assignee:

Spirit AeroSystems, Inc., Wichita, KS (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23K 20/233 (2006.01); F16B 5/08 (2006.01); B23K 20/10 (2006.01); B23K 20/12 (2006.01); B23K 26/323 (2014.01); B23K 9/23 (2006.01); B23K 20/06 (2006.01); B23K 31/02 (2006.01); B64F 5/00 (2017.01); B23K 101/00 (2006.01); B23K 103/20 (2006.01); B23K 103/18 (2006.01); B23K 103/10 (2006.01); B23K 101/34 (2006.01); B23K 103/16 (2006.01);
U.S. Cl.
CPC ...
B23K 20/2336 (2013.01); B23K 9/232 (2013.01); B23K 20/06 (2013.01); B23K 20/10 (2013.01); B23K 20/122 (2013.01); B23K 20/2333 (2013.01); B23K 26/323 (2015.10); B23K 31/02 (2013.01); B64F 5/00 (2013.01); B23K 2101/006 (2018.08); B23K 2101/34 (2018.08); B23K 2103/10 (2018.08); B23K 2103/166 (2018.08); B23K 2103/18 (2018.08); B23K 2103/20 (2018.08);
Abstract

A structure and a method of creating the structure in which relatively thin pieces of non-weldable aluminum alloy or other non-weldable material are welded together. First layers of a weldable material, such as a weldable aluminum alloy or other weldable material, having a total thickness of between 0.01 and 0.30 inches, are built up on a surface of the first piece using an ultrasonic or other solid state joining technique, and second layers of the weldable material having a similar total thickness are built up on a surface of the second piece using the same technique. The first piece is then welded to the second piece at the first and second layers of weldable material using a fusion welding technique. The resulting structure may be part of an aircraft, landcraft, watercraft, or spacecraft type of vehicle or may be used in other high-performance applications.


Find Patent Forward Citations

Misak, Heath. (2020). Structure and method of making same involving welding otherwise non-weldable materials (U.S. Patent No. 10661381). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10661381

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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