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:
Apr. 02, 2024

Filed:

Oct. 18, 2021
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Jeffrey Michael Olds, Seattle, WA (US);

Eric George Gruner, Seattle, WA (US);

Billy P. Tung, Seattle, WA (US);

Eric Dwight Blohm, Bellevue, WA (US);

Assignee:

The Boeing Company, Arlington, VA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 3/56 (2006.01); B64C 3/54 (2006.01); B64C 23/06 (2006.01);
U.S. Cl.
CPC ...
B64C 3/56 (2013.01); B64C 3/54 (2013.01); B64C 3/546 (2013.01); B64C 23/069 (2017.05);
Abstract

Apparatus and methods for limiting trailing edge deflection in aircraft folding wing tips are disclosed herein. An example aircraft wing disclosed herein includes a fixed wing portion. The fixed wing portion includes an outboard rib. The aircraft wing also includes a wing tip moveably coupled to the fixed wing portion. The wing tip is moveable between an extended position and a folded position. The wing tip includes an inboard rib that is disposed in a trailing edge section of the wing tip. The wing tip includes a stop plate coupled to the inboard rib. The stop plate extends inboard from the inboard rib such that when the wing tip is in the extended position, the stop plate is disposed below a portion of the outboard rib of the fixed wing portion to limit upward deflection of the trailing edge section of the wing tip relative to the fixed wing portion.


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