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. 04, 2025

Filed:

May. 17, 2022
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Guillaume Glemarec, Moissy-Cramayel, FR;

Bruno Albert Beutin, Moissy-Cramayel, FR;

Valerio Capasso, Moissy-Cramayel, FR;

Jean-Baptiste Manuel Nicolas Vignes, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/40 (2024.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
B64D 27/40 (2024.01); B64D 27/402 (2024.01); B64D 27/404 (2024.01); B64D 27/406 (2024.01); F01D 25/28 (2013.01);
Abstract

A structure for linking and supporting a turbine engine on an aircraft pylon, the structure having a first longitudinal axis intended to extend parallel to a second longitudinal axis of the pylon, the structure including a first axial portion for fastening to the pylon, the first portion having an upper end that defines a substantially horizontal plane of interface with the pylon, and a lower end bearing suspension rods for suspending the turbine engine, which extend in a rear vertical plane; and a second axial portion that is intended to extend forward of the pylon and includes at least one suspension member of the turbine engine in a front vertical plane.


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