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:
Jun. 05, 2018

Filed:

Dec. 04, 2015
Applicant:

Airbus Operations (Sas), Toulouse, FR;

Inventors:

Loic Dussol, Toulouse, FR;

Jerome Dane, Ventabren, FR;

Hugo Herisson, Roques sur Garonne, FR;

Assignee:

Airbus Operations (SAS), Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/54 (2006.01); F02K 1/82 (2006.01); F02K 1/72 (2006.01);
U.S. Cl.
CPC ...
F02K 1/827 (2013.01); F02K 1/72 (2013.01); F05D 2250/283 (2013.01); F05D 2260/963 (2013.01); Y02T 50/671 (2013.01);
Abstract

A thrust reverser for an aircraft engine assembly, comprising two sub-assemblies configured to surround an engine, each of the sub-assemblies comprising an inner fixed structure, a translating cowl, a torque box, a substantially vertical 12 o'clock bifurcation, and a substantially vertical 6 o'clock bifurcation. At least one of the sub-assemblies comprises at least one separating partition extending between the inner fixed structure, the translating cowl and the torque box of the sub-assembly, the separating partition being rigidly fixed to the inner fixed structure and the torque box, and connected to the translating cowl via a sliding connection.


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