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. 28, 2020

Filed:

Jun. 19, 2017
Applicant:

Airbus Operations Sas, Toulouse, FR;

Inventors:

Camil Negulescu, Toulouse, FR;

Jean-Michel Rogero, Toulouse, FR;

Renaud Faure, Blagnac, FR;

Assignee:

AIRBUS OPERATIONS SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/14 (2006.01); B64C 39/04 (2006.01); B64D 29/04 (2006.01); B64D 27/20 (2006.01); B64C 1/16 (2006.01); B64C 5/02 (2006.01); B64D 33/02 (2006.01); F02C 7/04 (2006.01); B64C 21/02 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64D 27/14 (2013.01); B64C 1/16 (2013.01); B64C 5/02 (2013.01); B64C 39/04 (2013.01); B64D 27/20 (2013.01); B64D 29/04 (2013.01); B64D 33/02 (2013.01); F02C 7/04 (2013.01); B64C 21/02 (2013.01); B64C 2001/0045 (2013.01); B64D 2033/0226 (2013.01); Y02T 50/44 (2013.01);
Abstract

In order to further benefit from the principle of boundary layer ingestion by engines of an aircraft assembly, the rear portion of the fuselage of this aircraft assembly includes a front portion which splits up into at least two distinct rear portions, spaced apart from each other, and each integrating the rotary ring of the receiver of one of the engines.


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