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:
Jun. 17, 2025

Filed:

Oct. 22, 2024
Applicant:

Honeywell International Inc., Charlotte, NC (US);

Inventors:

Antonin Skarolek, Brno, CZ;

Tomas Ripel, Brno, CZ;

Michal Nozka, Brno, CZ;

Assignee:

HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16H 63/34 (2006.01); B64C 13/34 (2006.01); F16H 57/10 (2006.01); F16H 1/28 (2006.01); F16H 3/46 (2006.01); F16H 48/10 (2012.01);
U.S. Cl.
CPC ...
B64C 13/34 (2013.01); F16H 57/10 (2013.01); F16H 63/34 (2013.01); F16H 1/2854 (2013.01); F16H 3/46 (2013.01); F16H 48/10 (2013.01); F16H 2048/104 (2013.01);
Abstract

A differential actuator system for controlling a flight control surface is provided, which includes a first control lane subsystem, a second control lane subsystem, a differential subsystem and a differential lock subsystem. The differential subsystem includes a first gear set forming a first load path from the first control lane to the flight control surface, and a second gear set forming a second load path from the second control lane to the flight control surface. The differential lock subsystem operably couples to the first gear set and the second gear set and is switchable between a locked state to couple the first and second gear sets in a torque-summing mode for moving the flight control surface and an unlocked state to couple the first and second gear sets in a velocity-summing mode for moving the flight control surface. Control signals issued from a controller operate the differential actuator system.


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