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:
Sep. 25, 2018

Filed:

Jun. 16, 2017
Applicants:

Airbus Operations (S.a.s.), Toulouse, FR;

Airbus (S.a.s.), Blagnac, FR;

Inventors:

Jerôme Bazile, Leguevin Toulouse, FR;

Patrice Rouquette, Pompertuzat, FR;

Matthias Eberle, Ulm, DE;

Philippe Perrin, Toulouse, FR;

Assignees:

Airbus Operations (S.A.S.), Toulouse, FR;

Airbus (S.A.S.), Blagnac, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/06 (2006.01); B64C 19/00 (2006.01); B64D 45/04 (2006.01); G05D 1/08 (2006.01); G05D 1/10 (2006.01); G05D 1/04 (2006.01); G08G 5/02 (2006.01); G08G 5/00 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0676 (2013.01); B64C 19/00 (2013.01); B64D 45/04 (2013.01); G05D 1/0825 (2013.01); G05D 1/101 (2013.01); G08G 5/0021 (2013.01); G08G 5/025 (2013.01); G05D 1/042 (2013.01);
Abstract

A method and device for assisting initiation of a flare maneuver of an aircraft during a landing. The device includes an acquisition unit for acquiring current values of flight parameters of the aircraft, including the current height of the aircraft with respect to the ground, a computation unit for computing a first reference height and a second reference height, corresponding to a height starting from which the aircraft attains a current start of flare height while maintaining its current descent conditions over a predetermined first duration and over a predetermined second duration respectively, and an acoustic emission unit for emitting at least two sound signals in the cockpit of the aircraft, namely a first sound signal when the current height of the aircraft attains the first reference height during the descent and a second sound signal when the current height of the aircraft attains the second reference height during descent.


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