公开(公告)号：US09019127B2

公开(公告)日：2015-04-28

申请号：US13868913

申请日：2013-04-23

Applicant: Thales

Inventor： Didier Gautheron ,  Chris Deseure ,  Xavier Chazottes ,  Patrick Serrot

IPC: G08B21/00 ,  B64F5/00 ,  G09B9/16 ,  G06F17/30 ,  G05B23/02

CPC classification number: B64F5/00 ,  G05B23/027 ,  G05B23/0272 ,  G06F17/30303 ,  G09B9/16

Abstract: A method to develop a system for management of warnings and electronic procedures for an aircraft, comprising a database of parameters relating to the warnings and to logic and procedures, the aircraft comprising ATA equipment, comprises definition and calculation of maturity criteria for development of the system, which comprises, in order: A) verification of warnings in the database with respect to predefined lists of warnings and calculation of a maturity criterion, B) if the criterion of A>predetermined threshold, verification of the coherence of the logic for the warnings then definition and calculation of a maturity criterion, C) if the criterion of B>predetermined threshold, verification of the existence of the procedures and, for each warning, analysis of its logic with respect to its procedure, then definition and calculation of a maturity criterion, the system being fully set up when the latter criterion>predetermined threshold.

Abstract translation: 一种开发用于管理飞机警告和电子程序的系统的方法，包括与警告相关的参数数据库以及逻辑和程序，包括ATA设备的飞机包括定义和计算系统开发的成熟度标准 ，其按顺序包括：A）根据预定义的警告列表和成熟度标准的计算，验证数据库中的警告，B）如果A>的标准>预定阈值，则验证警告逻辑的一致性 然后定义和计算成熟度标准，C）如果B>预定阈值的标准，验证程序的存在，并且对于每个警告，其逻辑对其程序的分析，然后定义和计算成熟度 标准，当后一标准>预定阈值时，系统完全建立。

公开(公告)号：US11955013B2

公开(公告)日：2024-04-09

申请号：US17236672

申请日：2021-04-21

Applicant: THALES

Inventor： Chris Deseure ,  Sébastien Boussiron ,  Yannick Le Roux

IPC: G08G5/00

CPC classification number: G08G5/0021 ,  G08G5/003 ,  G08G5/0047 ,  G08G5/0073

Abstract: This electronic configuration assist device of a flight of an aircraft includes:



an acquisition module configured to acquire a flight modality, previously selected by a user from a set of predefined flight modalities;
a determination module configured to determine a group of avionics functional component(s) as a function of the acquired modality, each functional component having an elementary score for each predefined flight modality, an overall score being calculated for each possible group of components from the elementary score or scores of the components of the said group for the acquired modality, the determined group being the one having the best overall score among the calculated overall scores;
a display module configured to display information relating to each component of the determined group of avionics functional component(s).

公开(公告)号：US11420730B2

公开(公告)日：2022-08-23

申请号：US16447533

申请日：2019-06-20

Applicant: THALES

Inventor： Sylvain Lissajoux ,  François Michel ,  Chris Deseure ,  Denis Bonnet

IPC: G05D1/00 ,  B64C19/02 ,  B64C13/02 ,  B64D45/00 ,  G08G5/00

Abstract: Methods and systems for assisting the piloting of an aircraft are provided. The system includes at least one avionics type system and at least one non-avionics type system. The method includes steps involving receiving avionics type data associated with a flying context of the aircraft; forwarding the avionics type data to a non-avionics type system or computer; determining, in the non-avionics computer, one or more adjustment recommendations for equipment based on the received flying context and/or on predetermined data; displaying one or more recommendations. Various developments are described, in particular the conditions for requesting and/or computing recommendations (e.g. ongoing adjustment of the avionics, similar previous configuration, etc.), the selection and the categorization of recommendations, the handling of adjustment data for the avionics, etc. Software aspects are described.

公开(公告)号：US10510243B2

公开(公告)日：2019-12-17

申请号：US16148834

申请日：2018-10-01

Applicant: THALES

Inventor： Chris Deseure ,  Laurent Flotte

IPC: G08B29/18 ,  G05B23/02 ,  G06F11/07 ,  G06F11/28 ,  B64D45/00

Abstract: A method for processing an error when performing a predetermined avionics procedure, related computer program and detection and alert system is disclosed. In one aspect, the method is carried out automatically by the detection and alert system of an aircraft, the method including monitoring the operation of one or several avionics device(s) of the aircraft, the monitoring based on the tracking of a sequence representative of the predetermined avionics procedure being carried out. The method further includes: detecting a break of the sequence due to an incorrect command and/or skipping of at least one expected command according to the predetermined avionics procedure being performed, and retrieving at least one piece of information representative of the break in the sequence.

公开(公告)号：US10569899B2

公开(公告)日：2020-02-25

申请号：US16141217

申请日：2018-09-25

Applicant: THALES

Inventor： Chris Deseure ,  Laurent Flotte ,  Guillaume Urbanski

IPC: G08B21/00 ,  B64D45/00 ,  G06Q10/06 ,  G06Q50/30 ,  B64F5/60 ,  G05B23/02

Abstract: The invention relates to a method for controlling the restitution of alert(s) and/or of system(s) reconfiguration procedure(s), including the surveillance of device(s) of a vehicle and the determination of alert(s) and/or of associated reconfiguration procedure(s) to be restituted for the crew, the vehicle operating according to a mission carried out by using at least one operational capacity, and further including, for a current mission: obtaining a list of operational capacities required by said current mission; from said required operational capacities and at least one piece of information from an accessible database, controlling the restitution of alert(s) and/or of system(s) reconfiguration procedure(s) by: modifying the associated level of alert(s) and/or of procedure(s), and sequencing the restitution of alert(s) and/or of procedure(s) based on said level, and/or filtering said alert(s) and/or reconfiguration procedure(s) before restitution.

公开(公告)号：US10358231B2

公开(公告)日：2019-07-23

申请号：US15344676

申请日：2016-11-07

Applicant: THALES

Inventor： Laurent Flotte ,  Chris Deseure ,  Guillaume Urbanski

IPC: B64D45/00 ,  B64D15/20 ,  B64D43/00 ,  G08G5/00 ,  G05B23/02

Abstract: This decision aid method includes the following steps: acquiring (110) operating states of systems, the operating states being determined by a monitoring system; determining (120) an availability state of each operational capacity, based on the operating states of only the systems of the aircraft implementing that operational capacity, each availability state being chosen from among the group consisting of: a normal state, a downgraded state, an impacted state and a lost state; selecting (150) one or more operational capacities based on the current movement context of the aircraft; communicating (150) the availability state of each selected operational capacity to the pilot.

公开(公告)号：US09950808B2

公开(公告)日：2018-04-24

申请号：US13869717

申请日：2013-04-24

Applicant: THALES

Inventor： Fabien Guilley ,  Chris Deseure ,  Gilles Francois

IPC: B64D45/00 ,  G06Q10/06

CPC classification number: B64D45/00 ,  G06F2209/543 ,  G06Q10/06

Abstract: A method and a device for configuring an alerts management system for an aircraft comprises: generating a list of a plurality of alerts and of resolution procedures for an aircraft; for each alert, defining: distinctive characteristics of the alert; logic for detecting the alert; at least one procedure for resolving the alert; and, for each alert, defining recording in a dedicated alerts file the set of information defined for said alert, the alerts file having a structure and a format of data that are predefined for the alerts and the procedures; determining existing links between the dedicated alerts files; and in response to the determining step, updating the content of the dedicated alerts files according to the links identified.