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:
Nov. 08, 2016

Filed:

Aug. 24, 2012
Applicants:

Mathieu Gaillot, Paris, FR;

Jean Bertucchi, Thiais, FR;

Matthieu Leyko, Melun, FR;

Inventors:

Mathieu Gaillot, Paris, FR;

Jean Bertucchi, Thiais, FR;

Matthieu Leyko, Melun, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/20 (2006.01); B64C 7/02 (2006.01); B64D 27/26 (2006.01);
U.S. Cl.
CPC ...
F02C 7/20 (2013.01); B64C 7/02 (2013.01); B64D 27/26 (2013.01); B64D 2027/266 (2013.01);
Abstract

In an assembly including a bypass turbine engine and an attachment system attaching the turbine engine to an aircraft structure, the attachment system includes a mast, at least two rear attachments connecting the mast to two rear attachment points of the turbine engine, and a rear covering covering the rear attachments and providing a streamlined fairing. The rear covering includes two side walls, each including a first portion extending along and in proximity of the mast and extending rearwards, and a second portion projecting sideways relative to the first portion towards its outside, to cover the rear attachments. Each second portion is substantially a bulge and is connected to the first portion along a curved connection line extending between front and rear points situated substantially level with an inner longitudinal edge of the first portion to minimize the impact on a flow of bypass stream leaving the bypass passage.


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