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:
Aug. 06, 2019

Filed:

Sep. 17, 2015
Applicant:

Airbus Operations S.l., Getafe, ES;

Inventors:

Nicolas Bailey Noval, Getafe, ES;

Raul Llamas Sandin, Getafe, ES;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/077 (2006.01); F02C 6/14 (2006.01); F02C 6/20 (2006.01); F02K 3/06 (2006.01); F02K 5/00 (2006.01);
U.S. Cl.
CPC ...
F02C 6/14 (2013.01); F02C 6/20 (2013.01); F02C 6/206 (2013.01); F02K 3/06 (2013.01); F02K 5/00 (2013.01); F05D 2220/323 (2013.01); F05D 2220/64 (2013.01); F05D 2220/76 (2013.01);
Abstract

A propulsion engine comprising at least a first propulsion unit including a first fan encased by a geared ring and a gas turbine engine driving a first shaft connected to the first fan, at least a second propulsion unit including a second fan encased by a geared ring connected to a second shaft operatively coupled to an electric machine and at least an electric storage device connected to the electric machine. The geared rings are configured to transmit torque between the fans so that they can rotate in conjunction (directly or through an intermediate gear) when they are driven by at least one of said first and second shafts. The propulsion engine is arranged for controlling the torque to be supplied to the assembly of the first and second fans by the gas turbine engine and/or by the electric machine acting as a motor or as a generator.


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