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. 11, 2022

Filed:

Mar. 11, 2019
Applicant:

Airbus Sas, Blagnac, FR;

Inventor:

Daniel Kierbel, Toulouse, FR;

Assignee:

AIRBUS SAS, Blagnac, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 5/10 (2006.01); B64C 5/02 (2006.01); B64C 9/02 (2006.01); B64C 9/06 (2006.01); B64C 5/06 (2006.01); B64C 1/26 (2006.01); B64C 5/00 (2006.01); B64C 9/00 (2006.01); B64C 27/82 (2006.01); B64C 3/56 (2006.01);
U.S. Cl.
CPC ...
B64C 5/10 (2013.01); B64C 1/26 (2013.01); B64C 5/00 (2013.01); B64C 5/02 (2013.01); B64C 5/06 (2013.01); B64C 9/00 (2013.01); B64C 9/02 (2013.01); B64C 9/06 (2013.01); B64C 3/56 (2013.01); B64C 2027/829 (2013.01);
Abstract

An aircraft comprising a fixed structure, a fuselage mounted on the fixed structure and a tail unit system comprising a structural element housed inside the fuselage and mounted to be rotationally mobile relative to the fixed structure about a transverse axis of rotation parallel to a transverse axis of the aircraft. A first actuation system displaces the structural element in rotation about the transverse axis of rotation, on either side of the structural element. A horizontal tail unit has one end rotationally mobiley mounted on the structural element about a longitudinal axis of rotation parallel to a longitudinal axis of the aircraft and another end which extends out of the fuselage by passing through a window in the fuselage. For each horizontal tail unit, a second actuation system displaces the horizontal tail unit in rotation about the longitudinal axis of rotation.


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