公开(公告)号：US20130282207A1

公开(公告)日：2013-10-24

申请号：US13869348

申请日：2013-04-24

Applicant: THALES

Inventor： Xavier CHAZOTTES ,  Stéphane BERTHEAU ,  Michel MAZENOUX

IPC: B64C19/00

CPC classification number: B64C19/00 ,  G05D1/0055 ,  G05D1/0825 ,  G06F17/00

Abstract: An alerts and procedures management system for an aircraft comprises a software kernel aboard the aircraft and a parameterization tool for the software kernel, which comprises a conversion module for converting a configuration file describing an operational need of the system into a database of binary parameters which is able to parameterize the software kernel. The software kernel comprises at least four elementary cells: a first cell for acquiring aircraft signals, a second cell for characterizing state variables of the aircraft, a third cell for computing at least one separate event, a fourth cell for scheduling the separate events for communication with the crew; each of the cells comprising a software engine parameterizable by the database.

Abstract translation: 飞机的警报和程序管理系统包括飞机上的软件内核和用于软件内核的参数化工具，其包括用于将描述系统的操作需要的配置文件转换成二进制参数的数据库的转换模块， 能够参数化软件内核。 软件内核包括至少四个基本单元：用于获取飞行器信号的第一单元，用于表征飞机的状态变量的第二单元，用于计算至少一个单独事件的第三单元，用于调度用于通信的单独事件的第四单元 与船员; 每个单元包括可由数据库参数化的软件引擎。

公开(公告)号：US20150187148A1

公开(公告)日：2015-07-02

申请号：US14565871

申请日：2014-12-10

Applicant: THALES

Inventor： Christian SANNINO ,  Xavier CHAZOTTES ,  Francois COULMEAU

IPC: G07C5/08 ,  B64D45/00

CPC classification number: G07C5/0808 ,  B64D45/00 ,  B64D2045/0085 ,  G05B23/0286 ,  G06F11/0739 ,  G06F11/0784 ,  G07C5/0841

Abstract: A device and method for assisting with reconfiguration of an aircraft, an aircraft including such a device and an associated computer program product are disclosed. In one aspect, the aircraft has an operational configuration, is configured to move in an operational environment, and includes at least one avionic system, at least one avionic member, and at least one monitoring system configured to detect an abnormality of an avionic member or a perturbation of the operational environment and to generate a fault information. The device is connected between at least one monitoring system and at least one avionic system, and includes a reception module configured to receive a fault information from the monitoring system, an impact computation module configured to compute an impact on the operational configuration of the aircraft, and a transmission module configured to transmit the computed impact to at least one avionic system.

Abstract translation: 公开了一种用于辅助重新配置飞行器的装置和方法，包括这种装置的飞机和相关联的计算机程序产品。 一方面，飞行器具有操作配置，被配置为在操作环境中移动，并且包括至少一个航空电子系统，至少一个航空电子部件和被配置为检测航空电子部件的异常的至少一个监视系统，或者 操作环境的扰动并产生故障信息。 该设备连接在至少一个监控系统和至少一个航空电子系统之间，并且包括被配置为从监控系统接收故障信息的接收模块，被配置为计算对飞行器的操作配置的影响的冲击计算模块， 以及传输模块，被配置为将所计算的冲击传递到至少一个航空电子系统。

公开(公告)号：US20130280679A1

公开(公告)日：2013-10-24

申请号：US13868913

申请日：2013-04-23

Applicant: THALES

Inventor： Didier GAUTHERON ,  Chris DESEURE ,  Xavier CHAZOTTES ,  Patrick SERROT

IPC: B64F5/00 ,  G06F17/30 ,  G09B9/16

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：US20130173090A1

公开(公告)日：2013-07-04

申请号：US13728731

申请日：2012-12-27

Applicant: THALES

Inventor： Camille RIEUNIER ,  Jerome SACLE ,  Joseph HUYSSEUNE ,  Xavier CHAZOTTES

IPC: G01C23/00

CPC classification number: G01C23/00 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0052

Abstract: A configured aircraft flight management aid system comprises: means of interpretation receiving data taken from external instructions from an external control center, data relating to aircraft equipment failures, cabin problems and problems related to the environment of the aircraft; means of determination receiving data from the means of interpretation and determining at least one reference constraint associated with at least one parameter representative of a flight path, a reference constraint associated with a reference parameter comprising a new constraint, different from the initial constraint when the item of data effectively necessitates following a new path, different from the initial path, and a reference constraint comprising the initial constraint when the means of determination do not have access to any data relating to an event effectively necessitating following a new path; warning means generating a warning to an operator when the path actually flown does not comply with said reference constraint.

Abstract translation: 配置的飞机飞行管理援助系统包括：从外部控制中心接收外部指令的数据的解释手段，与飞机设备故障有关的数据，客舱问题以及与飞机环境有关的问题; 确定从所述解释装置接收数据并确定与代表飞行路径的至少一个参数相关联的至少一个参考约束的装置，与包括新约束的参考参数相关联的参考约束，所述参考参数与所述初始约束不同，当所述项目 的数据有效地需要遵循与初始路径不同的新路径，以及包括初始约束的参考约束，当确定方法不能访问与事件相关的任何数据时，有效地需要跟随新路径; 当路径实际飞行不符合所述参考约束时，警告意味着向操作者产生警告。