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:
Feb. 17, 2026

Filed:

Jul. 24, 2023
Applicant:

The Boeing Company, Arlington, VA (US);

Inventors:

Patrick Mccormick, Mukilteo, WA (US);

Christopher Bujnowski, Everett, WA (US);

George Moy, Seattle, WA (US);

Sarah Sheehy, Shoreline, WA (US);

Endri Kerci, Mountlake Terrace, WA (US);

Austin Schantz, Everett, WA (US);

Paul Ryan Leonard, Seattle, WA (US);

Caitlin Boxell, Lancaster, CA (US);

Erin Campbell, Lake Forest Park, WA (US);

John W. Gunderson, Issaquah, WA (US);

Assignee:

THE BOEING COMPANY, Arlington, VA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64F 5/60 (2017.01); B64D 45/00 (2006.01); B64F 5/40 (2017.01); G06F 11/07 (2006.01); B64C 3/56 (2006.01);
U.S. Cl.
CPC ...
B64F 5/40 (2017.01); B64D 45/00 (2013.01); G06F 11/0739 (2013.01); G06F 11/079 (2013.01); B64C 3/56 (2013.01);
Abstract

A folding wingtip aircraft includes a wing that includes a primary portion and a wingtip. The folding wingtip aircraft includes a folding wingtip system configured to rotate the wingtip relative to the primary portion. The folding wingtip aircraft also includes a flight control computer. The flight control computer is configured to, in response to a first determination that a wingtip position of the wingtip is not in a folded position when a second determination indicates that a last completed command by the folding wingtip system was a fold command, set error codes for the folding wingtip system. The flight control computer is also configured to change a setting to indicate that the folding wingtip aircraft is grounded based on the error codes.


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