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:
May. 05, 2026

Filed:

Jun. 20, 2023
Applicant:

Safran Nacelles, Gonfreville-l'Orcher, FR;

Inventors:

Patrick Gonidec, Moissy-Cramayel, FR;

Loïc Chapelain;

Patrick André Boileau, Moissy-Cramayel, FR;

Assignee:

SAFRAN NACELLES, Gonfreville-l'Orcher, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); F02K 1/64 (2006.01); F02K 1/68 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); F02K 1/64 (2013.01); F02K 1/68 (2013.01);
Abstract

A thrust reverser () for an aircraft propulsion unit, the reverser comprising a stationary structure () and a movable structure () comprising at least one movable reverser cover () delimiting the secondary flow path (B), the movable structure being translatable with respect to the stationary structure between an advanced direct-thrust position and a retracted thrust-reversal position in which the movable structure () and the stationary structure () axially define therebetween, on the secondary flow path, a radial extraction opening () for at least one portion (B') of the secondary flow. The thrust reverser also comprises at least one deployable deflecting membrane () which is designed to deflect the at least one portion (B′) of the secondary flow forwards. Moreover, in the deployed configuration, the membrane () extends radially outwards beyond the movable reverser cover ().


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