公开(公告)号：US09014882B2

公开(公告)日：2015-04-21

申请号：US13886419

申请日：2013-05-03

Applicant: Airbus Operations SAS

Inventor： Anne Dumoulin ,  Marc Locheron

IPC: G06F19/00 ,  G08G5/02 ,  G05D1/06

CPC classification number: G08G5/02 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/025

Abstract: A device aiding the flight management of an aircraft during a phase of landing on an airport includes means for automatically determining an adaptive aiming point that is shifted along the runway in the downstream direction and which can be used by different usual landing aid means of the aircraft.

Abstract translation: 在机场着陆阶段期间协助飞机管理的装置包括用于自动确定沿下游方向沿着跑道移动的适应性瞄准点的装置，并且可由飞行器的不同常规着陆援助装置使用 。

公开(公告)号：US20130304285A1

公开(公告)日：2013-11-14

申请号：US13886419

申请日：2013-05-03

Applicant: Airbus Operations SAS

Inventor： Anne Dumoulin ,  Marc Locheron

IPC: G08G5/02

CPC classification number: G08G5/02 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/025

Abstract: A device aiding the flight management of an aircraft during a phase of landing on an airport includes means for automatically determining an adaptive aiming point that is shifted along the runway in the downstream direction and which can be used by different usual landing aid means of the aircraft.

Abstract translation: 在机场着陆阶段期间协助飞机管理的装置包括用于自动确定沿下游方向沿着跑道移动的适应性瞄准点的装置，并且可由飞行器的不同常规着陆援助装置使用 。

公开(公告)号：US12050154B2

公开(公告)日：2024-07-30

申请号：US16199615

申请日：2018-11-26

Applicant: Airbus Operations SAS ,  Airbus SAS

Inventor： Marc Locheron ,  Stéphane Lebru

IPC: G01M3/00 ,  B64D13/06 ,  B64D47/00 ,  B64F5/60 ,  G01F23/296 ,  G01M3/24 ,  G01M3/32

CPC classification number: G01M3/007 ,  B64D47/00 ,  B64F5/60 ,  G01F23/296 ,  G01M3/24 ,  G01M3/3263 ,  B64D2013/0618

Abstract: A method and a system for detecting leak noise in an aircraft, making it possible to perform ground tests in complete safety and over an entire cabin pressurization range, thus avoiding having to resort to a plurality of in-flight tests. The system includes: at least one acquisition device configured to be installed in at least one area of interest of the aircraft, the acquisition device being configured to acquire data in relation to current noise in the area of interest and data in relation to a current pressure gradient between the cabin of the aircraft and the outside, and a monitoring device configured to control the acquisition of the data by the at least one acquisition device and to receive the acquisition data in order to detect any leak noise in the at least one area of interest.

公开(公告)号：US20240118172A1

公开(公告)日：2024-04-11

申请号：US18376116

申请日：2023-10-03

Applicant: Airbus Operations SAS

Inventor： Marc Locheron ,  Fabien Roux-Portalez ,  Clothilde Martini ,  Emmanuel Helffer ,  Maxime Jouan ,  Adil Soubki

IPC: G01M17/00 ,  G01H17/00

CPC classification number: G01M17/00 ,  G01H17/00 ,  B64D2045/0085

Abstract: An aircraft sound diagnostic method includes a step of measurement of acoustic signals by a plurality of microphones mounted at different positions inside the aircraft, a step of recording of the measured acoustic signals, a computation step which generates a sound mapping on the basis of the measured acoustic signals, a step of comparison of the sound mapping and a reference mapping and a step of transmission of the comparison to a user device. The method makes it possible to track the trending of an abnormal noise or of an abnormal noise level and assist in determining the context thereof. An aircraft sound diagnostic device for implementing the method is also described.