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:
Jul. 02, 2019

Filed:

Dec. 18, 2014
Applicant:

Airbus Operations (S.a.s.), Toulouse, FR;

Inventors:

Julien Guillemaut, Toulouse, FR;

Sébastien Alby, Tournefeuille, FR;

Jérôme Colmagro, Toulouse, FR;

Pascal Pome, Cepet, FR;

Jonathan Blanc, Blagnac, FR;

Thomas Robiglio, Toulouse, FR;

Tobias Sjostrom, Toulouse, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64D 27/20 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64D 27/20 (2013.01); B64D 2027/262 (2013.01);
Abstract

In order to reduce engine deformation, the subject matter disclosed herein provides an assembly for an aircraft, comprising an aircraft rear section, an engine, a nacelle, and a mounting strut for mounting the engine on the rear section, the assembly also comprising mounting for mounting the engine on a rigid structure of the strut, the mounting comprising two engine mounts designed to react the axial thrust forces generated by the engine. According to the subject matter disclosed herein, the rigid structure of the strut comprises a first portion partially enveloping the engine, this first portion comprising an external skin forming part of an external aerodynamic surface of the nacelle, and the two engine mounts are arranged diametrically opposite each other at the rear of the rigid structure, being attached to the first portion.


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