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公开(公告)号:US09709982B2
公开(公告)日:2017-07-18
申请号:US14553191
申请日:2014-11-25
Applicant: AIRBUS OPERATIONS (SAS)
Inventor: Jean-Claude Mere , Pierre Neri , Julien Bernat , Marc Vie
IPC: H04L29/00 , G05D1/00 , G08G5/00 , G01C21/00 , G01C23/00 , G05D1/02 , G08G5/06 , H04L12/26 , H04L29/06 , H04L29/08 , G06Q10/08
CPC classification number: G05D1/00 , G01C21/00 , G01C23/00 , G05D1/0202 , G05D1/101 , G06Q10/06 , G06Q10/087 , G08G5/0021 , G08G5/003 , G08G5/0034 , G08G5/0039 , G08G5/06 , H04L43/0823 , H04L63/08 , H04L67/12
Abstract: A flight management system with core and supplementary modules is proposed. The core module may include generic applications that implement generic functionalities related to a flight management of the aircraft. The supplementary module may include supplementary applications that implement supplementary functionalities specific to an entity to which the aircraft belongs. The supplementary module may be divided into principal and auxiliary partitions (or entities), and the supplementary applications, also referred to as principal applications, may be implemented in the principal partition. One or more auxiliary applications may be implemented in the auxiliary partition. Each auxiliary application may be associated with one or more principal applications such that the execution of the principal application requires the associated auxiliary application to be executed.
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公开(公告)号:US09323248B2
公开(公告)日:2016-04-26
申请号:US14553274
申请日:2014-11-25
Applicant: AIRBUS OPERATIONS (SAS)
Inventor: Jean-Claude Mere , Pierre Neri , Julien Bernat , Marc Vie
IPC: G05D1/00 , G08G5/00 , G05D1/02 , G08G5/06 , H04L12/26 , H04L29/06 , H04L29/08 , G01C21/00 , G01C23/00 , G06Q10/08
CPC classification number: G05D1/00 , G01C21/00 , G01C23/00 , G05D1/0202 , G05D1/101 , G06Q10/06 , G06Q10/087 , G08G5/0021 , G08G5/003 , G08G5/0034 , G08G5/0039 , G08G5/06 , H04L43/0823 , H04L63/08 , H04L67/12
Abstract: A mission management system to manage both ground and flight phases of a mission of an aircraft is proposed. The mission management system may be implemented in flight management system architecture with core and supplementary modules distinct from each other. The core module may implement a set of generic functionalities related to a flight management of the aircraft, and the supplementary module may implement supplementary functionalities specific to an entity to which the aircraft belongs. The mission management system may include a flight management unit to define and manage a flight plan and associated flight trajectory, an airport navigation unit to define and manage a ground plan and associated ground trajectory, and a mission management unit to manage a continuity between the ground and flight phases of the mission and prediction computations made by the flight management and the airport navigation units.
Abstract translation: 提出了管理飞机任务的地面和飞行阶段的任务管理系统。 任务管理系统可以在具有彼此不同的核心和补充模块的飞行管理系统架构中实现。 核心模块可以实现与飞行器的飞行管理相关的一组通用功能,并且补充模块可以实现飞机所属实体特有的附加功能。 任务管理系统可以包括飞行管理单元来定义和管理飞行计划和相关联的飞行轨迹,机场导航单元来定义和管理地面计划和相关联的地面轨迹,以及任务管理单元来管理地面之间的连续性 飞行管理部门和机场导航部门的任务飞行阶段和预测计算。
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公开(公告)号:US11565822B2
公开(公告)日:2023-01-31
申请号:US16708760
申请日:2019-12-10
Applicant: Airbus Operations SAS
Inventor: Philippe Auge , Benoit Orteu , Julien Bernat , Jean Geliot , Delphine Jalbert , Frédéric Ridray , Laurent Lafont , Pascal Gardes
Abstract: A propulsion assembly having a pylon, a turbomachine comprising an engine and a fan that is enclosed by a fan casing, a nacelle surrounding the engine and the fan casing and having a load support disposed in the top part of the nacelle, a front engine attachment between the pylon and a front part of the engine, a rear engine attachment between the pylon and a rear part of the engine, a front fan attachment between the fan casing and the load support, and a rear pylon attachment between the pylon and the load support. Such a propulsion assembly allows a reduction in bulk since the load of the turbojet engine is distributed between the load support and the pylon, and the pylon is attached to the engine.
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公开(公告)号:US09529356B2
公开(公告)日:2016-12-27
申请号:US14553345
申请日:2014-11-25
Applicant: AIRBUS OPERATIONS (SAS)
Inventor: Jean-Claude Mere , Pierre Neri , Julien Bernat , Marc Vie
IPC: H04L29/00 , G05D1/00 , G08G5/00 , G05D1/02 , G08G5/06 , H04L12/26 , H04L29/06 , H04L29/08 , G01C21/00 , G01C23/00 , G06Q10/08
CPC classification number: G05D1/00 , G01C21/00 , G01C23/00 , G05D1/0202 , G05D1/101 , G06Q10/06 , G06Q10/087 , G08G5/0021 , G08G5/003 , G08G5/0034 , G08G5/0039 , G08G5/06 , H04L43/0823 , H04L63/08 , H04L67/12
Abstract: A system to manage transmissions of data between a flight management system (e.g., of an avionics type) of an aircraft and a portable electronic (e.g., of an open world type) is proposed. The data management system may be implemented in flight management system architecture with core and supplementary modules that are distinct from each other. The core module may implement a set of generic functionalities related to a flight management of the aircraft, and the supplementary module may implement supplementary functionalities specific to an entity to which the aircraft belongs. The data management system may comprise a data securing module that monitors data to be transmitted between the flight management system and the portable electronic device, and allows or prevents the data transmission based on the monitoring results.
Abstract translation: 提出了一种用于管理飞行器的飞行管理系统(例如,航空电子设备类型)和便携式电子设备(例如,开放式世界类型)之间的数据传输的系统。 数据管理系统可以在具有彼此不同的核心和补充模块的飞行管理系统架构中实现。 核心模块可以实现与飞行器的飞行管理相关的一组通用功能,并且补充模块可以实现飞机所属实体特有的附加功能。 数据管理系统可以包括数据保护模块,其监视在飞行管理系统和便携式电子设备之间要发送的数据,并且允许或防止基于监视结果的数据传输。
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公开(公告)号:US10216180B2
公开(公告)日:2019-02-26
申请号:US15422002
申请日:2017-02-01
Applicant: AIRBUS OPERATIONS (SAS)
Inventor: Jean-Claude Mere , Pierre Neri , Julien Bernat , Marc Vie
IPC: G05D1/10 , G08G5/00 , G05D1/00 , G05D1/02 , G08G5/06 , H04L12/26 , H04L29/06 , H04L29/08 , G01C21/00 , G01C23/00 , G06Q10/08 , G06Q10/06
Abstract: A flight management system architecture with separate core and supplementary modules. In the core module, generic functionalties relative to the flight management of the aircraft are implemented. In the supplementary module, supplementary functions are implemented. The supplementary functionalities include functionalties specific to an entity to which the aircraft belongs such as the specific aircraft model, a family of aircraft, a company, an alliance, and so on. The flight management system also includes a message exchange interface in which enables the core and supplementary modules to exchanges messages with each other. The core and supplementary modules includes corresponding core module and supplementary module interfacing functionaltities that respectively interface with generic and specific man-machine interfaces.
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公开(公告)号:US09606534B2
公开(公告)日:2017-03-28
申请号:US14552822
申请日:2014-11-25
Applicant: AIRBUS OPERATIONS (SAS)
Inventor: Jean-Claude Mere , Pierre Neri , Julien Bernat , Marc Vie
IPC: G05D1/00 , G08G5/00 , G05D1/02 , G08G5/06 , H04L12/26 , H04L29/06 , H04L29/08 , G01C21/00 , G01C23/00 , G06Q10/08
CPC classification number: G05D1/00 , G01C21/00 , G01C23/00 , G05D1/0202 , G05D1/101 , G06Q10/06 , G06Q10/087 , G08G5/0021 , G08G5/003 , G08G5/0034 , G08G5/0039 , G08G5/06 , H04L43/0823 , H04L63/08 , H04L67/12
Abstract: A flight management system architecture with two separate modules is proposed. In the core module, generic functionalities relative to the flight management of the aircraft are implemented. In the supplementary module, supplementary functions are implemented. The supplementary functionalities include functionalities specific to an entity to which the aircraft belongs such as the specific aircraft model, a family of airdraft, a company, an alliance, and so on. The flight management system also includes a message exchange interface in which enables the core and supplementary modules to exchanges messages with each other. The core and supplementary modules includes corresponding core module and supplementary module interfacing functionalities that respectively interface with generic and specific man-machine interfaces.
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