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:
Dec. 19, 2017

Filed:

Dec. 18, 2014
Applicant:

Airbus Operations (Sas), Toulouse, FR;

Inventors:

Alain Porte, Colomiers, FR;

Matthieu Fargues, Montauban, FR;

Assignee:

Airbus Operations (SAS), Toulouse, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F01D 25/00 (2006.01); B64D 33/02 (2006.01); B64D 29/00 (2006.01);
U.S. Cl.
CPC ...
F01D 25/24 (2013.01); B64D 29/00 (2013.01); B64D 33/02 (2013.01); F01D 25/005 (2013.01); B64D 2033/0286 (2013.01);
Abstract

An aircraft turbojet engine nacelle comprising an air intake assembly of substantially annular shape, the air intake assembly comprising an external wall and an internal wall which are connected to one another upstream by an air intake lip and downstream by an annular rear structure. The annular rear structure comprises, arranged concentrically, one or more monolithic panels forming a first annular zone and comprising one or more hollow casings forming at least a second annular zone, and at least one connecting ring which provides the connection with at least one of the external and internal walls. The annular rear structure thus has increased structural mechanical strength.


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