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:
Feb. 06, 2024

Filed:

Mar. 18, 2021
Applicant:

Safran Nacelles, Gonfreville l'Orcher, FR;

Inventors:

François Bellet, Moissy Cramayel, FR;

Jérôme Corfa, Moissy Cramayel, FR;

Julien Van Den Driessche, Moissy Cramayel, FR;

Assignee:

Safran Nacelles, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); F02K 1/763 (2013.01); F05D 2220/323 (2013.01); F05D 2260/52 (2013.01); F05D 2270/051 (2013.01);
Abstract

A turbofan engine nacelle includes a thrust reverser system provided with at least one movable cowl retracting towards a rear reverse-jet position, tilting pivoting flaps which at least partially close an annular flow duct, and opening lateral openings of this annular flow duct equipped with reverser grids. Each movable cowl includes a control sector that slides in a transverse plane, a deflection device linking a fixed part of the nacelle to this control sector in order to make it slide towards a reversal position when the movable cowl retracts, and flap connecting rods linking this control sector to the pivoting flaps, which tilt these flaps, closing the annular flow duct, when the control sector slides towards its reversal position.


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