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. 26, 2018

Filed:

Sep. 17, 2015
Applicant:

Airbus Operations S.l., Madrid, ES;

Inventors:

Nicolas Bailey Noval, Madrid, ES;

Raul Llamas Sandin, Madrid, ES;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/107 (2006.01); F16H 1/20 (2006.01); F02K 3/06 (2006.01); F02K 3/077 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 3/107 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F02K 3/077 (2013.01); F16H 1/20 (2013.01); F05D 2220/32 (2013.01); F05D 2260/4031 (2013.01);
Abstract

A multi-fan engine including a gas turbine engine, a casing and fans encased by geared rings, which connect with the geared rings of an adjacent fan(s) such that the rotation of one fan rotates the other fans. Intermediate gears may prove the connection between adjacent geared rings, wherein the intermediate gears are retracted by linear actuators to disengage the intermediate gears from the geared rings and thereby disengage the fans from each other. The multi-fan engine may be mounted flush to the fuselage of an aircraft invention to capture into the fans boundary layer airflow moving over the skin of the fuselage.


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