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.

Patent No.:

US 10190605 B1

PDF
Full Text
Expired
Date of Patent:
Jan. 29, 2019

Filed:

Jun. 18, 2018
Applicant:

Safran Nacelles, Gonfreville L'Orcher, FR;

Inventor:

Vincent Le Coq, Gonfreville L'Orcher, FR;

Assignee:

Safran Nacelles, Gonfreville L'Orcher, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/76 (2006.01); F15B 15/06 (2006.01); F15B 11/22 (2006.01); F15B 15/26 (2006.01); F02K 1/09 (2006.01); F02K 1/15 (2006.01);
U.S. Cl.
CPC ...
F15B 15/063 (2013.01); F02K 1/09 (2013.01); F02K 1/15 (2013.01); F02K 1/763 (2013.01); F15B 11/22 (2013.01); F15B 15/261 (2013.01); F05D 2220/323 (2013.01); F05D 2270/64 (2013.01); F15B 2211/7107 (2013.01); F15B 2211/72 (2013.01); F15B 2211/782 (2013.01); Y02T 50/671 (2013.01);
Abstract

The present disclosure concerns a nacelle for an aircraft turbojet engine that includes a thrust reverser having a cowl displaceable between a deployed position and a stowed position, a fixed structure, and a secondary nozzle. The nozzle includes panels movable in rotation, and hydraulic actuators for sequenced actuation of the cowl and panels. The actuators include a body mounted on the fixed structure, and a rod mounted in the body and is linked to the cowl and panels via a device for transmitting movement of the actuator to the panel. An actuation system having a hydraulic control device controls the displacement of the rod of the actuator. The actuator further includes a device for alternately displacing the rod in translation relative to the body to cause translation of the cowl, or in rotation relative to the body to cause rotation of the nozzle panel.


Find Patent Forward Citations

Le Coq, Vincent. (2019). Nacelle for an aircraft turbojet engine provided with a hydraulic roto-linear actuator of a thrust reverser and of a variable-section nozzle (U.S. Patent No. 10190605). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10190605

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

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