公开(公告)号：US10082799B2

公开(公告)日：2018-09-25

申请号：US15625285

申请日：2017-06-16

Applicant: AIRBUS OPERATIONS (S.A.S.) ,  AIRBUS (S.A.S.)

Inventor： Jerôme Bazile ,  Patrice Rouquette ,  Matthias Eberle ,  Philippe Perrin

IPC: G05D1/06 ,  B64C19/00 ,  B64D45/04 ,  G05D1/08 ,  G05D1/10 ,  G05D1/04 ,  G08G5/02 ,  G08G5/00

CPC classification number: G05D1/0676 ,  B64C19/00 ,  B64D45/04 ,  G05D1/042 ,  G05D1/0825 ,  G05D1/101 ,  G08G5/0021 ,  G08G5/025

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.

公开(公告)号：US10908292B2

公开(公告)日：2021-02-02

申请号：US16143714

申请日：2018-09-27

Applicant: Airbus Operations S.A.S.

Inventor： Jerôme Bazile ,  Patrice Rouquette ,  Sylvain Raynaud ,  Nicolas Marconnet ,  Guillaume Discours ,  Kevin Etchebarne

IPC: G01S19/15 ,  B64D45/04 ,  G01S1/02 ,  G01S1/18 ,  G08G5/02 ,  G01S13/91 ,  G01S1/16 ,  G05D1/06

Abstract: The system for aiding the landing of an aircraft on a landing runway of an airport equipped with an Instrument Landing System (“ILS”) corresponding to an axis of a predetermined approach, includes: an ILS signals receiver and a processing unit. The processing unit is configured to, when the ILS signals receiver) has not yet captured a Glide signal corresponding to a Glide axis of the approach as a function of items of information relating to the predetermined approach, acquired from a database, determine a protection volume in which there is no risk of the ILS signals receiver detecting a replica of the Glide signal; and when a current position of the aircraft is above the protection volume, inhibit the capture of the Glide signal by the ILS signals receiver and instruct the emission of an alert item of information in the cockpit of the aircraft.

公开(公告)号：US20190113593A1

公开(公告)日：2019-04-18

申请号：US16143714

申请日：2018-09-27

Applicant: Airbus Operations S.A.S.

Inventor： Jerôme Bazile ,  Patrice Rouquette ,  Sylvain Raynaud ,  Nicolas Marconnet ,  Guillaume Discours ,  Kevin Etchebarne

IPC: G01S1/02 ,  G01S1/18 ,  G01S1/16 ,  G01S13/91 ,  G08G5/02

Abstract: The system for aiding the landing of an aircraft on a landing runway of an airport equipped with an Instrument Landing System (“ILS”) corresponding to an axis of a predetermined approach, includes: an ILS signals receiver and a processing unit. The processing unit is configured to, when the ILS signals receiver) has not yet captured a Glide signal corresponding to a Glide axis of the approach as a function of items of information relating to the predetermined approach, acquired from a database, determine a protection volume in which there is no risk of the ILS signals receiver detecting a replica of the Glide signal; and when a current position of the aircraft is above the protection volume, inhibit the capture of the Glide signal by the ILS signals receiver and instruct the emission of an alert item of information in the cockpit of the aircraft.