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:
Jul. 07, 2026

Filed:

Jul. 06, 2023
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Hugues Barbier, Moissy-Cramayel, FR;

Sébastien Oriol, Moissy-Cramayel, FR;

Kevin Didier Pierre Le Normand, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F15B 11/08 (2006.01); B64C 11/38 (2006.01); F02K 1/66 (2006.01); F02K 1/76 (2006.01); F15B 20/00 (2006.01); B64C 11/30 (2006.01);
U.S. Cl.
CPC ...
F15B 11/08 (2013.01); B64C 11/38 (2013.01); F02K 1/66 (2013.01); F02K 1/763 (2013.01); F02K 1/766 (2013.01); F15B 20/002 (2013.01); F15B 20/004 (2013.01); B64C 11/30 (2013.01); F05D 2220/323 (2013.01); F05D 2260/74 (2013.01); F15B 2211/30525 (2013.01); F15B 2211/30565 (2013.01); F15B 2211/329 (2013.01); F15B 2211/6316 (2013.01); F15B 2211/862 (2013.01); F15B 2211/863 (2013.01); F15B 2211/8636 (2013.01); F15B 2211/8752 (2013.01); F15B 2211/8757 (2013.01);
Abstract

A hydraulic control circuit of a steering actuator having a first and a second chamber, for orienting the blades of an aircraft engine propeller, this circuit comprising a high-pressure line and a low-pressure line, a first protection valve being able to assume a deactivated position or an activated position for placing the first chamber in communication with the high-pressure line, a second protection valve being able to assume a deactivated position or an activated position for placing the second chamber in communication with the low-pressure line, each protection valve comprising a hydraulic activation inlet and a hydraulic deactivation inlet which can be pressurised in order to activate or deactivate these valves. The circuit includes a solenoid protection valve controlling an amplification valve connected to the inlets of the protection valves in order to activate them upon the activation of the solenoid protection valve.


Find Patent Forward Citations

Barbier, Hugues. (2026). Protection for a circuit for controlling the orientation of propeller blades of an aircraft engine (U.S. Patent No. 12674475). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12674475

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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