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:
Nov. 10, 2026

Filed:

Dec. 17, 2025
Applicant:

The Boeing Company, Arlington, VA (US);

Inventors:

Navid Daneshvaran, Everett, WA (US);

Takao Suzuki, Mill Creek, WA (US);

Kim Marie Larson, Olalla, WA (US);

Jeffrey Peter Baucum, Sequim, WA (US);

Assignee:

THE BOEING COMPANY, Arlington, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/24 (2006.01); B64C 9/02 (2006.01);
U.S. Cl.
CPC ...
B64C 9/24 (2013.01); B64C 9/02 (2013.01); B64C 2230/14 (2013.01);
Abstract

An aircraft wing assembly configured to reduce aerodynamic noise generated by leading-edge slats during high-lift operations. The assembly may include a fixed wing portion, a leading-edge slat having a noise-suppressing projection on a cove surface, a projection receiving portion configured to receive the noise-suppressing projection when the leading-edge slat is in a retracted position, and a surface portion configured to move between a first position in which the surface portion at least partially defines the projection receiving portion and a second position in which the surface portion moves to provide a convex or planar surface in place of the projection receiving portion. The surface portion may be configured to move to the first position when the leading-edge slat is in a retracted position and is configured to move to the second position when the leading-edge slat is in an extended position.


Find Patent Forward Citations

Quick Actions:

Daneshvaran, Navid. (2026). Aircraft wing configured to reduce aerodynamic noise generated by leading-edge slats during high-lift operations (U.S. Patent No. 12789978). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12789978

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