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    MANAGEMENT OF AN AIRCRAFT
    1.
    发明申请
    MANAGEMENT OF AN AIRCRAFT 审中-公开

    公开(公告)号：US20190389565A1

    公开(公告)日：2019-12-26

    申请号：US16447533

    申请日：2019-06-20

    Applicant: THALES

    Inventor： Sylvain LISSAJOUX ,  François MICHEL ,  Chris DESEURE ,  Denis BONNET

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

    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.

    FLIGHT MANAGEMENT SYSTEM FOR AN AIRCRAFT
    2.
    发明公开
    FLIGHT MANAGEMENT SYSTEM FOR AN AIRCRAFT 审中-公开

    公开(公告)号：US20240321118A1

    公开(公告)日：2024-09-26

    申请号：US18605710

    申请日：2024-03-14

    Applicant: THALES

    Inventor： Frédéric BONAMY ,  Baptiste IDIART ,  Baptiste LEFEVRE ,  François MICHEL ,  Olivier SOUSSIEL

    IPC: G08G5/00 ,  G08G5/04

    CPC classification number: G08G5/0039 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/045

    Abstract: A flight management system for an aircraft, includes a critical first avionics module for trajectory calculation, i.e. a module the integrity level and availability level of which are specified by regulatory standards in force, delivering as output a safe trajectory, based on a flight plan; a second module for trajectory calculation that is less critical than the critical first module, i.e. a module the integrity level and availability level of which are lower than those of the first module, delivering as output an improved trajectory that is less safe than the trajectory delivered by the critical first avionics module, based on a flight plan; a critical avionics module for trajectory verification, configured to validate or invalidate the safety of the less safe improved trajectory; and a critical avionics module for decision-making configured to select a trajectory from the safe trajectory and the less safe trajectory.

    SYSTEM FOR AIDING THE GUIDANCE OF AN AIRCRAFT TRAVELLING AROUND AN AIRPORT ZONE
    3.
    发明申请
    SYSTEM FOR AIDING THE GUIDANCE OF AN AIRCRAFT TRAVELLING AROUND AN AIRPORT ZONE 有权
    用于援引机场行驶的飞机指导系统

    公开(公告)号：US20140249739A1

    公开(公告)日：2014-09-04

    申请号：US13857976

    申请日：2013-04-05

    Applicant: Thales

    Inventor： Stéphanie LAFON ,  François MICHEL

    IPC: G08G5/04 ,  G08G5/06

    CPC classification number: G08G5/04 ,  G08G5/0021 ,  G08G5/0078 ,  G08G5/065

    Abstract: The general field of the invention is that of systems for aiding the guidance of a first aircraft travelling around an airport zone. The system according to the invention comprises: a set of databases comprising bulkiness and performance characteristics of the said first aircraft, geometric and technical characteristics of the airport zone and information about the air traffic in the immediate environment of the said first aircraft; calculation means making it possible to firstly determine a safety zone around the said first aircraft taking into account at least the position of the said aircraft, its size and the uncertainty in the measurement of its position; and then a taxiing indication on the basis of the information arising from the databases and the characteristics of the safety zone; viewing means displaying at least one view of the airport zone in which the first aircraft is situated and a representation of the said taxiing indication.

    Abstract translation: 本发明的一般领域是用于帮助驾驶机场区域周围的第一架飞机的辅助系统。 根据本发明的系统包括：一组数据库，包括所述第一飞行器的蓬松性和性能特征，机场区域的几何和技术特征以及关于在所述第一飞行器的直接环境中的空中交通的信息; 计算意味着可以首先确定所述第一飞机周围的安全区域，至少考虑所述飞机的位置，其尺寸和其位置的测量中的不确定性; 然后根据数据库提供的信息和安全区的特点制定滑行指示; 显示第一飞机所在的机场区域的至少一个视图的观看装置和所述滑行指示的表示。

    Method and electronic device for managing the execution of software application services on an avionics platform, related computer program and avionics system
    5.
    发明申请
    Method and electronic device for managing the execution of software application services on an avionics platform, related computer program and avionics system 有权

    公开(公告)号：US20250094216A1

    公开(公告)日：2025-03-20

    申请号：US18884112

    申请日：2024-09-13

    Applicant: THALES

    Inventor： Pierre HARAMBILLET ,  Guillaume CALLEWAERT ,  François MICHEL

    IPC: G06F9/48

    Abstract: A method of managing the execution of software services on an avionics platform including resources for the execution of the services is implemented by an electronic device and includes acquisition of contextual data for a group of software services to be executed, the contextual data including, for each software service: a maximum number of resources used by the service, an operating requirement of the service equal to resistance to breakdown/s or non-resistance to breakdown/s, and, if the operating requirement of the service is equal to resistance to breakdown/s, a number of breakdown/s the service should withstand, computation, from the acquired contextual data, of a context for the group of software services, and launching of the execution of software service/s of the group according to a set of distribution rule/s of the services and depending upon the computed context.

    METHOD OF ALLOCATION IN AN ON-BOARD DATA TRANSMISSION NETWORK IN A MOBILE PASSENGER TRANSPORT VEHICLE AND ASSOCIATED COMPUTER PROGRAM
    6.
    发明申请
    METHOD OF ALLOCATION IN AN ON-BOARD DATA TRANSMISSION NETWORK IN A MOBILE PASSENGER TRANSPORT VEHICLE AND ASSOCIATED COMPUTER PROGRAM 有权

    公开(公告)号：US20230126393A1

    公开(公告)日：2023-04-27

    申请号：US17973265

    申请日：2022-10-25

    Applicant: THALES

    Inventor： François MICHEL ,  Pierre HARAMBILLET ,  Pierre BOULLET

    IPC: H04B7/185 ,  H04W72/04 ,  H04W24/02 ,  H04W16/22

    Abstract: The present invention relates to an allocation method in a transmission network on-board a mobile vehicle, the network comprising wireless access points configured for transmitting and receiving, over a functioning channel, radio signals between said access point and a plurality of terminals.
    The method comprising the following steps: provision of a digital model of the mobile vehicle and of the access points; for every available channel and for every access point, simulation of the propagation of signals from said access point on said available channel; for every available channel, for every access point and for every terminal, determination of an estimated associated bandwidth according to the simulation; allocation of one of the available channels and one of the access points to every terminal according to the estimated bandwidths.

    METHOD FOR DETERMINING AN INSTANTANEOUS OR ANTICIPATED PROBABLE ZONE OF OCCUPANCY OF AN AIRCRAFT IN AN AIRPORT NAVIGATION ZONE
    8.
    发明申请
    METHOD FOR DETERMINING AN INSTANTANEOUS OR ANTICIPATED PROBABLE ZONE OF OCCUPANCY OF AN AIRCRAFT IN AN AIRPORT NAVIGATION ZONE 有权
    确定机场航行区航空器的即时或预期可能的可能区域的方法

    公开(公告)号：US20140236470A1

    公开(公告)日：2014-08-21

    申请号：US13857979

    申请日：2013-04-05

    Applicant: Thales

    Inventor： Stéphanie LAFON ,  François MICHEL

    IPC: G08G5/04 ,  G08G5/00

    CPC classification number: G08G5/04 ,  G08G5/0065 ,  G08G5/065

    Abstract: The general field of the invention is that of methods for determining safety zones surrounding an aircraft travelling or taking off from an airport zone, the safety zone being calculated at a determined instant that may be the present instant or the future instant. The method according to the invention comprises at least the following steps: Step 0: Establishment of a convex safety envelope surrounding the aircraft on the basis of reference points taken on the aircraft; Step 1: Establishment of a first convex envelope safety zone surrounding the aircraft on the basis of reference circles taken on the aircraft, each circle having as centre one of the reference points and as radius the value of the uncertainty in the exact position of the aircraft. Other steps of the method make it possible to refine this first safety zone depending on whether the aircraft is in a taxiing or takeoff phase and depending on whether it is calculated at the present instant or at the future instant.

    Abstract translation: 本发明的一般领域是用于确定围绕从机场区域行驶或起飞的飞行器的安全区域的方法，安全区域在可能是当前时刻或未来时刻的确定时刻计算。 根据本发明的方法至少包括以下步骤：步骤0：根据飞机上的参考点建立围绕飞行器的凸形安全信封; 步骤1：根据飞机上的参考圆，建立围绕飞机的第一个凸包安全区，每个圆圈以参考点为中心，并以飞机确切位置的不确定度值为半径 。 该方法的其他步骤使得可以根据飞行器是否处于滑行或起飞阶段并且取决于是在当前时刻还是在未来时刻计算来完善该第一安全区域。

    FLIGHT MANAGEMENT SYSTEM OF AN AIRCRAFT
    9.
    发明申请
    FLIGHT MANAGEMENT SYSTEM OF AN AIRCRAFT 有权

    公开(公告)号：US20250014468A1

    公开(公告)日：2025-01-09

    申请号：US18677005

    申请日：2024-05-29

    Applicant: THALES

    Inventor： Frédéric BONAMY ,  Baptiste IDIART ,  Baptiste LEFEVRE ,  François MICHEL ,  Olivier SOUSSIEL

    IPC: G08G5/00 ,  G06N3/02

    Abstract: A flight management system of an aircraft includes a first non-critical or open world module for creating an enhanced enriched flight plan, the first module being configured to create the enhanced enriched flight plan iteratively by the following steps: initialisation of pseudo-constraints; and iterative enhancement of the choice of pseudo-constraints, until an objective of enhancement or of absence of enhancement with respect to the last best choice of pseudo-constraints is reached, based on at least one optimisation criterion and on at least one parameter representative of the environment of the flight of the aircraft; the second critical or flight management avionics module certified to calculate a path, comprising at least one critical computer and/or at least one critical piece of software for calculating and delivering as output a secured path, based on the enhanced enriched flight plan supplied by the first module.

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