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, 2020

Filed:

Jul. 19, 2017
Applicant:

Safran Nacelles, Gonfreville l'Orcher, FR;

Inventors:

Patrick Boileau, Tournefeuille, FR;

Olivier Kerbler, Antony, FR;

Julien Lezerac, Toulouse, FR;

Armel Gautier, Negrepelisse, FR;

Loïc Grall, Elancourt, FR;

Ludovic Toupet, Alfortville, FR;

Assignee:

SAFRAN NACELLES, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); B64D 29/06 (2006.01); F02C 7/20 (2006.01); B64D 27/26 (2006.01); B64D 27/16 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); B64D 27/16 (2013.01); B64D 27/26 (2013.01); B64D 29/06 (2013.01); F01D 25/24 (2013.01); F02C 7/20 (2013.01); B64D 2027/264 (2013.01); F05D 2220/323 (2013.01); F05D 2260/50 (2013.01);
Abstract

The present disclosure provides a nacelle rear assembly for turbojet engine including at least one thrust reverser device to redirect air flow circulating from upstream to downstream in a flow path of the turbojet engine and a mast to link the nacelle to a structure of the aircraft. In one form, the nacelle extends longitudinally from forth to back along an axis and includes a cradle fastened on the mast. In one form, the cradle includes a first longeron and a second longeron extending longitudinally on either side of the mast. The first and second longeron each include a sliding guide device for sliding of a movable cowl and of a cascade of the thrust reverser device.


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