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:
Jan. 31, 2023

Filed:

Dec. 10, 2019
Applicant:

Airbus Operations Sas, Toulouse, FR;

Inventors:

Philippe Auge, Brax, FR;

Benoit Orteu, Toulouse, FR;

Julien Bernat, Toulouse, FR;

Jean Geliot, Toulouse, FR;

Delphine Jalbert, Toulouse, FR;

Frédéric Ridray, L'Isle Jourdain, FR;

Laurent Lafont, Pechbusque, FR;

Pascal Gardes, Levignac, FR;

Assignee:

AIRBUS OPERATIONS SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64D 27/18 (2006.01); B64D 29/06 (2006.01); F02C 7/20 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64D 27/18 (2013.01); B64D 29/06 (2013.01); B64D 2027/266 (2013.01); B64D 2027/268 (2013.01); F02C 7/20 (2013.01); F02K 3/06 (2013.01);
Abstract

A propulsion assembly having a pylon, a turbomachine comprising an engine and a fan that is enclosed by a fan casing, a nacelle surrounding the engine and the fan casing and having a load support disposed in the top part of the nacelle, a front engine attachment between the pylon and a front part of the engine, a rear engine attachment between the pylon and a rear part of the engine, a front fan attachment between the fan casing and the load support, and a rear pylon attachment between the pylon and the load support. Such a propulsion assembly allows a reduction in bulk since the load of the turbojet engine is distributed between the load support and the pylon, and the pylon is attached to the engine.


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