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:
Feb. 22, 2022

Filed:

Oct. 03, 2018
Applicant:

Airbus Operations Sas, Toulouse, FR;

Inventors:

Frederic Journade, Toulouse, FR;

Eric Bouchet, Aussonne, FR;

Olivier Barbara, Puylaurens, FR;

Pascal Pome, Cepet, FR;

Assignee:

AIRBUS OPERATIONS SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64D 27/18 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64D 27/18 (2013.01); B64D 2027/268 (2013.01);
Abstract

An aircraft engine assembly has a front engine mount connecting an engine and a primary structure of a pylon comprising at least one front rod having at least three front link points. A first front link point is configured to connect the front rod and the front end of the primary structure. A second front link point is configured to connect the front rod and the core of the engine. A third front link point is configured to connect the front rod and the engine core and is offset relative to the second front link point in a horizontal transverse direction. The first front link point of the front engine mount is separated from the rotation axis of the engine by a distance greater than an exterior radius of the rear casing of the core of the engine at the rear link point of the rear engine mount.


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