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:
Oct. 20, 2020

Filed:

Nov. 09, 2017
Applicants:

Airbus Operations Gmbh, Hamburg, DE;

Airbus Operations S.l., Getafe, ES;

Inventors:

Daniel Reckzeh, Hamburg, DE;

Raul Carlos Llamas Sandin, Getafe, ES;

Assignees:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); B64C 5/02 (2006.01); B64C 7/02 (2006.01); B64D 27/26 (2006.01); B64D 27/20 (2006.01);
U.S. Cl.
CPC ...
B64D 33/02 (2013.01); B64C 5/02 (2013.01); B64C 7/02 (2013.01); B64D 27/20 (2013.01); B64D 27/26 (2013.01); B64D 2033/0226 (2013.01); Y02T 50/40 (2013.01);
Abstract

An aircraft comprising a fuselage extending along a longitudinal axis between a fore section and an aft section, wings mounted to the fuselage, a tail unit mounted to the aft section of the fuselage, and a first propulsion unit and a second propulsion unit both mounted to the aft section of the fuselage in such a way that a first axis of rotation of the first propulsion unit and a second axis of rotation of the second propulsion unit both extend in a vertical center plane spanned by the longitudinal axis and a yaw axis. The provided centerline mounted double-engine aircraft allows for a simple manufacture, maintenance and retrofit of the engines, in that the first propulsion unit and/or the second propulsion unit are arranged outside the fuselage.


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