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:
Nov. 02, 2021

Filed:

Feb. 13, 2019
Applicant:

Airbus Operations Sas, Toulouse, FR;

Inventors:

Pascal Gardes, Levignac, FR;

Frédéric Ridray, L'Isle Jourdain, FR;

Frédéric Piard, Tournefeuille, FR;

José Goncalves, Colomiers, FR;

Assignee:

Airbus Operations SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 29/06 (2006.01); F02K 1/80 (2006.01); F02K 1/72 (2006.01); B64D 27/18 (2006.01); F02K 3/06 (2006.01); B64D 29/02 (2006.01); F02K 1/62 (2006.01); B64D 29/04 (2006.01); F02K 1/64 (2006.01); F02K 1/70 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
B64D 29/06 (2013.01); B64D 27/18 (2013.01); B64D 29/02 (2013.01); B64D 29/04 (2013.01); F02K 1/625 (2013.01); F02K 1/64 (2013.01); F02K 1/70 (2013.01); F02K 1/72 (2013.01); F02K 1/80 (2013.01); F02K 3/06 (2013.01); F01D 25/28 (2013.01); F05D 2240/14 (2013.01); F05D 2260/30 (2013.01);
Abstract

A turbojet engine comprising an engine, a nacelle comprising a fan case, an intermediate case having a part forming a hub and an outer shroud radially spaced away from the hub by a secondary, or bypass, flow path and fixed to the hub via arms, in which the outer shroud is situated to the rear and in the continuity of the fan case, a fixed structure fixed to the outer shroud, a mobile assembly mounted with the ability to effect translational movement on the fixed structure, and a ramp fixed to the outer shroud and configured to direct the secondary or bypass flow to exit the outer shroud. Such a turbojet engine makes it possible to simplify assembly and among other things, makes it possible to fix the ramp directly to the outer shroud.


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