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. 03, 2026

Filed:

Dec. 12, 2023
Applicant:

Thales, Meudon, FR;

Inventors:

Jean-Claude Bourland, Chatellerault, FR;

Gérard Simon-Bouhet, Chatellerault, FR;

Gilles Thouvenot, Valence, FR;

Assignee:

THALES, Meudon, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/50 (2006.01); B64C 13/10 (2006.01); B64C 13/18 (2006.01); F16D 55/226 (2006.01); F16D 59/00 (2006.01); F16D 65/38 (2006.01); F16D 65/46 (2006.01); F16F 15/03 (2006.01);
U.S. Cl.
CPC ...
B64C 13/505 (2018.01); B64C 13/10 (2013.01); B64C 13/18 (2013.01); F16D 55/226 (2013.01); F16D 59/00 (2013.01); F16D 2065/383 (2013.01); F16D 65/46 (2013.01); F16F 15/035 (2013.01);
Abstract

A flight control actuator for providing assistance to means for piloting an aircraft is provided. This flight actuator includes an electric motor, an input shaft suitable for being rotated by the electric motor, the input shaft including an input clutch device, the input clutch device having an active position wherein it is capable of coupling the input shaft to an output shaft via an intermediate shaft, and an inactive position. The output shaft is capable of being connected to the apparatus or method for piloting the aircraft, the output shaft being suitable for being coupled to the input shaft when the input clutch device is in the active position. The actuator includes a backup assistance shaft, the backup assistance shaft being suitable for being coupled to the output shaft when the input clutch device is in the inactive position.


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Bourland, Jean-Claude. (2026). Mechanical control actuator for an aircraft (U.S. Patent No. 12780405). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12780405

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