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:
Mar. 03, 2026

Filed:

Sep. 07, 2023
Applicant:

The Boeing Company, Arlington, VA (US);

Inventors:

Eric S. Kamila, Tukwila, WA (US);

Ramon A. Burin, Seattle, WA (US);

John A. Standley, Seattle, WA (US);

Assignee:

The Boeing Company, Arlington, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/22 (2006.01); B64C 9/02 (2006.01); B64C 13/40 (2006.01); F15B 15/14 (2006.01);
U.S. Cl.
CPC ...
B64C 9/22 (2013.01); B64C 9/02 (2013.01); B64C 13/40 (2013.01); F15B 15/14 (2013.01);
Abstract

An aircraft wing includes a fixed structure and a linear hydraulic slat actuator attached to the fixed structure. The linear hydraulic slat actuator is oriented spanwise along the aircraft wing. The aircraft wing also includes an actuator output link and a slat attached to the actuator output link. The aircraft wing also includes a bell-crank coupled to the linear hydraulic slat actuator and to the actuator output link. In response to spanwise movement of the linear hydraulic slat actuator, the bell-crank is configured to move the actuator output link in a different direction that enables the slat to move between a retracted position and an extended position.


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