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. 01, 2008

Filed:

Nov. 24, 2004
Applicants:

Stéphane Machado, Villeneuve-Tolosane, FR;

Jérôme Cassagne, Toulouse, FR;

Anthony Del Blanco, Toulouse, FR;

Yvon Martin, Bonrepos Riquet, FR;

Arnaud Chambreuil, Labastide St Sernin, FR;

Inventors:

Stéphane Machado, Villeneuve-Tolosane, FR;

Jérôme Cassagne, Toulouse, FR;

Anthony Del Blanco, Toulouse, FR;

Yvon Martin, Bonrepos Riquet, FR;

Arnaud Chambreuil, Labastide St Sernin, FR;

Assignee:

Airbus France, Toulouse, FR;

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

This invention relates to a structure () for mounting an engine () under an aircraft wing (), comprising a rigid structure () and means () of mounting this rigid structure under the wing, the mounting means () comprising a forward fastener () and an aft fastener (). According to the invention, the forward fastener has at least one triangular shackle on each side of a vertical plane passing through a longitudinal axis () of the engine, placed in a vertical plane oriented along a direction inclined with respect to a longitudinal direction (X) and a transverse direction (Y) of the aircraft, and located in a horizontal plane defined by these directions (X) and (Y). Furthermore, the aft fastener comprises at least one shackle oriented along a vertical direction (Z) of the aircraft.


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