logo

For the Inventor, By the Inventor

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.

Patent No.:

US 12290852 B1

PDFFull Text
Date of Patent:
May. 06, 2025

Filed:

Jul. 20, 2023

Autonomous flexible manufacturing system for building a fuselage

Applicant:

The Boeing Company, Arlington, VA (US);

Inventors:

Harinder S. Oberoi, Snohomish, WA (US);

Branko Sarh, Huntington Beach, CA (US);

Melissa Ann Findlay, Snohomish, WA (US);

Alan S. Draper, Everett, WA (US);

Jorge Alberto Arriaga, Kirkland, WA (US);

Richard Griffith Reese, Iv, Seattle, WA (US);

Alfredo Jose Gerosa, Snohomish, WA (US);

Kevin Marion Barrick, Kingston, WA (US);

Michael J. Kozak, Snohomish, WA (US);

Quang T. Do, Mukilteo, WA (US);

Jeffrey Lawrence Miller, Mukilteo, WA (US);

Yuanxin Charles Hu, Newcastle, WA (US);

Assignee:

The Boeing Company, Arlington, VA (US);

Attorney:

Yee & Associates, P.C.

Primary Examiner:

Christopher J Besler

Int. Cl.
CPC ...
B64F 5/10 (2016.12); B21J 15/02 (2005.12); B21J 15/10 (2005.12); B21J 15/14 (2005.12); B21J 15/28 (2005.12); B21J 15/32 (2005.12); B21J 15/40 (2005.12); B23P 19/10 (2005.12); B25B 5/16 (2005.12); B25J 5/00 (2005.12); B25J 9/16 (2005.12); B25J 11/00 (2005.12); B29C 39/02 (2005.12); B29C 39/10 (2005.12); B29C 39/12 (2005.12); B29C 39/22 (2005.12); B29C 45/14 (2005.12); B29C 65/70 (2005.12); B60G 3/14 (2005.12); B60G 7/00 (2005.12); B64C 1/00 (2005.12); B64C 1/06 (2005.12); B64F 5/50 (2016.12); F16B 19/06 (2005.12); G05B 19/418 (2005.12); G05D 1/00 (2005.12); G05D 3/12 (2005.12); B23P 21/00 (2005.12); B29L 31/00 (2005.12); B60P 3/025 (2005.12);
U.S. Cl.
CPC ...
B21J 15/28 (2012.12); B21J 15/02 (2012.12); B21J 15/10 (2012.12); B21J 15/142 (2012.12); B21J 15/32 (2012.12); B21J 15/40 (2012.12); B23P 19/10 (2012.12); B25B 5/163 (2012.12); B25J 5/007 (2012.12); B25J 9/1682 (2012.12); B25J 9/1687 (2012.12); B25J 9/1697 (2012.12); B25J 11/005 (2012.12); B25J 11/007 (2012.12); B29C 39/026 (2012.12); B29C 39/10 (2012.12); B29C 39/123 (2012.12); B29C 39/22 (2012.12); B29C 45/14336 (2012.12); B29C 65/70 (2012.12); B60G 3/145 (2012.12); B60G 7/001 (2012.12); B60G 7/008 (2012.12); B64C 1/00 (2012.12); B64C 1/06 (2012.12); B64C 1/068 (2012.12); B64F 5/10 (2016.12); B64F 5/50 (2016.12); F16B 19/06 (2012.12); G05B 19/41805 (2012.12); G05D 1/0088 (2012.12); G05D 3/12 (2012.12); B23P 21/002 (2012.12); B23P 2700/00 (2012.12); B23P 2700/01 (2012.12); B29C 2045/14368 (2012.12); B29C 2793/0081 (2012.12); B29K 2715/00 (2012.12); B29L 2031/748 (2012.12); B60G 2204/143 (2012.12); B60G 2204/418 (2012.12); B60G 2206/8207 (2012.12); B60G 2300/60 (2012.12); B60P 3/025 (2012.12); B64C 1/069 (2012.12); G05B 2219/45071 (2012.12); Y02P 90/80 (2015.10); Y10S 901/01 (2012.12); Y10S 901/02 (2012.12); Y10S 901/41 (2012.12);
Abstract

A method and apparatus for building a fuselage assembly for an aircraft. A number of fixtures may be drive across a floor to an assembly area to form an assembly fixture. The fuselage assembly may be built on the assembly fixture.

Find Patent Forward Citations

Loading…