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. 03, 2017

Filed:

Jan. 25, 2016
Applicants:

Airbus (Sas), Blagnac, FR;

Airbus Operations (Sas), Toulouse, FR;

Inventors:

Philippe Perrin, Toulouse, FR;

Matthias Eberle, Tournefeuille, FR;

Assignee:

Airbus Operations (SAS), Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 45/04 (2006.01); B64D 47/02 (2006.01); B64D 45/00 (2006.01); G05D 1/06 (2006.01); G05D 1/08 (2006.01); G08G 5/00 (2006.01); G08G 5/02 (2006.01);
U.S. Cl.
CPC ...
B64D 45/04 (2013.01); B64D 45/0005 (2013.01); B64D 47/02 (2013.01); G05D 1/0676 (2013.01); G05D 1/085 (2013.01); G08G 5/0021 (2013.01); G08G 5/025 (2013.01);
Abstract

A device for assisting in the landing of an aircraft in a flare phase comprising a control stick, a first unit for acquiring current flight parameters of the aircraft, a second unit for acquiring a current deflection angle of the control stick, a computation unit for computing a difference between the current deflection angle of the control stick and a target deflection angle of the control stick, and an acoustic emission unit configured to automatically emit a warning or guidance sound signal in the cockpit of the aircraft, according to the difference between the current deflection angle and the target deflection angle of the control stick.


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