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:
May. 19, 2015

Filed:

Feb. 27, 2009
Applicants:

Frédéric Journade, Toulouse, FR;

Laurent Lafont, Pechbusque, FR;

Delphine Jalbert, Seilh, FR;

Inventors:

Frédéric Journade, Toulouse, FR;

Laurent Lafont, Pechbusque, FR;

Delphine Jalbert, Seilh, FR;

Assignee:

AIRBUS OPERATIONS S.A.S., Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/20 (2006.01); B64D 27/26 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64D 2027/264 (2013.01); F01D 25/28 (2013.01); F02C 7/20 (2013.01); Y02T 50/672 (2013.01);
Abstract

An aircraft engine assembly including an attachment mechanism of a turbojet onto a rigid structure of a mounting strut, including a first, second, and third forward engine attachment for taking up thrust loads brought onto the fan frame, and arranged such that the third attachment passes through a first diametrical plane of the turbojet, the first and second attachments being disposed on one side and another of the first plane. The first and second forward engine attachments are respectively brought to the fan frame at two points, situated beyond the second diametrical plane of the turbojet, orthogonal to the first diametrical plane, with respect to the third attachment.


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