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:
Sep. 01, 2020

Filed:

Nov. 01, 2017
Applicant:

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

Inventors:

Jean Pierre Couffignal, Blagnac, FR;

Jérôme Cassagne, Toulouse, FR;

Didier Rovatti, Toulouse, FR;

Thomas Deforet, Toulouse, FR;

Benoit Orteu, Toulouse, FR;

Michael Belin, Castelginest, FR;

Miren Egana-Abarrategui, Toulouse, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64D 45/00 (2013.01); B64D 2027/266 (2013.01); B64D 2027/268 (2013.01); B64D 2045/0085 (2013.01);
Abstract

A rear engine attachment includes a beam attached to the reactor strut, a rudder mounted by a pivot connection on the beam about a main rotational axis, and two thrust rods each exhibiting a first end attached to the rudder and a second end attached to a front section of an engine, the two thrust rods and the rudder attached to the beam together defining a primary thrust path between the engine and the reactor strut to bear the engine thrust. For each thrust rod, the rear engine attachment exhibits a waiting fail-safe system activated in the event of a failure of the primary thrust path. The rear engine attachment includes, for each thrust rod, a break detector integral with the rudder which is provided to come into contact with the beam in the event of a failure of the primary thrust path. The attachment allows a quick inspection to be made to determine whether there has been a failure of the primary thrust path.


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