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. 04, 2014

Filed:

Sep. 20, 2010
Applicants:

Frederic Journade, Toulouse, FR;

Laurent Lafont, Pechbusque, FR;

Laurent Agostini, La Salvetat Saint Gilles, FR;

Eric Renaud, Brignemont, FR;

Delphine Jalbert, Seilh, FR;

Inventors:

Frederic Journade, Toulouse, FR;

Laurent Lafont, Pechbusque, FR;

Laurent Agostini, La Salvetat Saint Gilles, FR;

Eric Renaud, Brignemont, FR;

Delphine Jalbert, Seilh, FR;

Assignee:

Airbus Operations S.A.S., Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

An engine is suspended from a main linear portion of a structure mounted on a fuselage or a wing surface of an aircraft. A connection includes flat symmetrical wings at an angle to one another, to support an attaching flange on which the engine is mounted, directly or through a mounting element. The flat shape of the wings makes them easy to manufacture, and enables them to resist the forces satisfactorily. The intermediate element resists overhang forces of the mounting satisfactorily. Flexible connections filter the engine's vibrations and prevent irregular forces being transmitted.


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