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:
Jan. 05, 2021

Filed:

Oct. 13, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Erin Ahern, Seattle, WA (US);

Tom Mark Balut, Renton, WA (US);

Gary Bond, Kent, WA (US);

Bryan Jacob Gruner, Bellevue, WA (US);

Eric Milligan, Seattle, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 9/16 (2006.01); B64C 3/18 (2006.01); B64C 9/02 (2006.01);
U.S. Cl.
CPC ...
B64C 3/187 (2013.01); B64C 3/185 (2013.01); B64C 9/02 (2013.01); B64C 9/16 (2013.01);
Abstract

Aircraft wings having improved deflection control ribs are described. An example aircraft wing includes a rear spar, an outboard flap, a rear spar fitting, and a deflection control rib. The outboard flap is movable relative to the rear spar between a stowed position and a deployed position. The outboard flap includes a closure rib and a roller coupled to the closure rib. The rear spar fitting is coupled to the rear spar. The deflection control rib includes a primary arm and a catch. The primary arm is coupled to and extends rearward from the rear spar fitting proximate a lower surface of the aircraft wing. The catch is coupled to and extends rearward from the primary arm. The catch includes an opening to receive the roller of the outboard flap when the outboard flap is in the stowed position.


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