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:
Apr. 04, 2023

Filed:

Sep. 18, 2020
Applicants:

Safran Nacelles, Gonfreville l'Orcher, FR;

Safran Aircraft Engines, Paris, FR;

Inventors:

Quentin Garnaud, Moissy-Cramayel, FR;

Guillaume Glemarec, Moissy-Cramayel, FR;

Patrick Boileau, Rond-Point René Ravaud Réau, FR;

Ludovic Toupet, Moissy-Cramayel, FR;

Assignees:

Safran Nacelles, Gonfreville l'Orcher, FR;

Safran Aircraft Engines, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); B64D 29/08 (2006.01); B64D 29/06 (2006.01); B64D 7/02 (2006.01); B64C 1/14 (2006.01); B64C 7/02 (2006.01); F02K 1/80 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); B64C 1/1446 (2013.01); B64C 7/02 (2013.01); B64D 29/06 (2013.01); B64D 29/08 (2013.01); F02K 1/80 (2013.01); F05D 2220/323 (2013.01);
Abstract

A turbofan propulsion assembly includes a thrust reverser with movable flaps. The propulsion assembly further includes an engine and a nacelle surrounding the engine, and the nacelle includes a thrust reverser with sliding cowls and thrust reverser flaps, and an inner structure. The portion of the inner structure positioned perpendicular to the thrust reverser flaps includes two halves that can open toward the exterior of the nacelle cowls.


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