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1. 外观设计

USD752102S1 Display screen with an icon 有权
公开(公告)号：USD752102S1
公开(公告)日：2016-03-22
申请号：US29494800
申请日：2014-06-24
申请人： THALES Avionics SAS
设计人： Patrick Mazoyer , Sonia Vautier , Bertrand Caudron De Coquereaumont

2. 发明授权

US09709991B2 Management of the energy in an approach trajectory 有权
公开(公告)号：US09709991B2
公开(公告)日：2017-07-18
申请号：US14885866
申请日：2015-10-16
申请人： THALES
发明人： Valérie Bataillon , Sonia Vautier , Emmanuel Dewas
IPC分类号： G05D1/06 , G08G5/00 , G08G5/02 , G01C21/20 , G05D1/10
CPC分类号： G05D1/0676 , G01C21/20 , G05D1/0005 , G05D1/101 , G08G5/0039 , G08G5/006 , G08G5/025
摘要： A method implemented by computer for calculating a lateral approach trajectory of an aircraft, comprises the steps of receiving selection of a landing runway; determining a zone Z1, the zone defining trajectory limits to carry out a last turn with a view to landing on the indicated runway; receiving indication of a trajectory point FF defining a point of alignment of the aircraft; determining a joining trajectory bound for a point FAF2, the joining trajectory going from the aircraft to the point FAF2 and then to the point FF and then to the indicated landing runway without passing through the zone Z1. Developments describe the use of a zone Z2 associated with visibility conditions, the calculation of the energy to be dissipated, the use of a predefined descent profile, the emission of alerts and trajectory adaptations by increasing the length of the joining trajectory or use of the airbrakes.

3. 发明授权

US09524571B2 Method for assisting the navigation of an aircraft with correlation of dynamic information with a 4D flight trajectory 有权
标题翻译：用于协助航空器导航的方法，其具有与4D飞行轨迹的动态信息的相关性
公开(公告)号：US09524571B2
公开(公告)日：2016-12-20
申请号：US14712796
申请日：2015-05-14
申请人： THALES
发明人： François Coulmeau , Sonia Vautier , Frédéric Bonamy
IPC分类号： G01C21/00 , G01C23/00 , G06T11/20 , B64D43/00 , G09G5/36
CPC分类号： G06T11/206 , B64D43/00 , G01C21/00 , G01C23/005 , G06T2210/32 , G06T2210/61 , G09G5/36 , G09G2380/12
摘要： A method for assisting the navigation of an aircraft comprises: assembly by families of data by a processing unit of predetermined data and acquired data, including meteorological data, the families being predefined, each data value being associated with a time window of validity; formatting the data of the families to associate with each data value a type of graphical representation as text or a scalar, vector, surface, or volume; selection of families of data to be displayed; choice of a display time window for each family of data to be displayed; spatio-temporal discretization of the trajectory; spatio-temporal correlation of the discretized trajectory with each family of data as a function of the time windows of validity, in the display time windows of the family, to extract a sub-assembly from each family of data, by the processing unit; display of the sub-assemblies in a single representation on the same display screen.
摘要翻译：一种辅助航空器导航的方法包括：由预定数据的处理单元组合数据的数据，以及所获取的数据，包括气象数据，预定义的系列，每个数据值与有效时间窗口相关联; 将家族的数据格式化为与每个数据值相关联的一种图形表示作为文本或标量，向量，表面或体积; 选择要显示的数据族; 选择要显示的每个数据系列的显示时间窗口; 轨迹的时空离散化; 通过处理单元，在家庭的显示时间窗口中从每个数据系列提取子组件，将离散轨迹与每个数据系列作为时间窗的函数的时空相关性; 在同一显示屏幕上以单个表示形式显示子组件。

4. 发明授权

US10026327B2 Managing the trajectory of an aircraft in case of engine outage 有权
公开(公告)号：US10026327B2
公开(公告)日：2018-07-17
申请号：US15344775
申请日：2016-11-07
申请人： THALES
发明人： Franck Prenot , Sonia Vautier , Philippe Chaix
IPC分类号： B64D45/00 , G08G5/00
摘要： A method for managing the trajectory of an aircraft implemented by computer comprises the steps consisting of: receiving the aeroplane performance levels, receiving a flight plan, receiving ground relief data, receiving weather data, determining the coordinates of a safety point according to the aeroplane performance levels, the relief data and the weather data, the safety point making it possible to continue the flight according to a predefined SID landing trajectory in case of outage of one or more engines of the aircraft. Developments are described, notably in computation of the spatial coordinates of the safety point, the management of several safety points and/or of EOSID trajectories, the insertion or the activation of an EOSID trajectory including in the absence of engine outage, the management of the Disarm Point flight plan point. System and software aspects are described.

5. 外观设计

USD791183S1 Display screen with an icon 有权
公开(公告)号：USD791183S1
公开(公告)日：2017-07-04
申请号：US29494802
申请日：2014-06-24
申请人： THALES Avionics SAS
设计人： Patrick Mazoyer , Sonia Vautier , Bertrand Caudron De Coquereaumont

6. 外观设计

USD752103S1 Display screen with an icon 有权
公开(公告)号：USD752103S1
公开(公告)日：2016-03-22
申请号：US29494805
申请日：2014-06-24
申请人： THALES Avionics SAS
设计人： Patrick Mazoyer , Sonia Vautier , Bertrand Caudron De Coquereaumont

7. 发明授权

US11195420B2 Method and system for assisting in the flight management of an aircraft in terms of optimizing the operating costs of said aircraft 有权
公开(公告)号：US11195420B2
公开(公告)日：2021-12-07
申请号：US16003649
申请日：2018-06-08
申请人： THALES
发明人： Xavier Blanchon , Guillaume Boyer , Guillaume Meulle , Sonia Vautier
IPC分类号： G08G5/00 , G01C21/20 , G05D1/06 , G05D1/00 , G01C23/00 , G05D1/10
摘要： A method for assisting in a flight management of an aircraft calculates a local cost function CF(xi, hj) at various altitudes hj along a planned vertical reference flight trajectory over a discrete set of points P(xi, hj) which forms a two-dimensional grid in which the planned vertical reference flight trajectory varies, the local cost function CF(xi, hj) being calculated locally at each point P(xi, hj) according to aircraft data and environmental data predicted at said local point P(xi, hj). Then, for each point P(xi, hj) of the grid, the method determines a neighbourhood including the point P(xi, hj), and associates a colour K(xi, hj) therewith that is dependent on the value of the local cost function CF(xi, hj) using a predetermined bijective lookup transformation. Next, the method displays the coloured grid formed by the coloured neighbourhoods.

8. 发明授权

US09530322B2 Contextual aid to flight management 有权
标题翻译：对飞行管理的情境援助
公开(公告)号：US09530322B2
公开(公告)日：2016-12-27
申请号：US14862431
申请日：2015-09-23
申请人： THALES
发明人： Bertrand Caudron , Sonia Vautier , Patrick Mazoyer
IPC分类号： G08G5/00 , B64D45/00 , G01C23/00 , G01D7/00 , G08G5/02
CPC分类号： G08G5/0039 , B64D45/00 , B64D2045/0075 , G01C23/005 , G01D7/00 , G08G5/0021 , G08G5/0047 , G08G5/0052 , G08G5/0065 , G08G5/025
摘要： A method implemented by computer for the management of the flight of an aircraft comprises the steps of receiving flight directives and flight information associated with these directives; determining a flight context of the aircraft; as a function of the context determined, selecting information from among that associated with the formulation of a directive and/or with a current flight directive and/or with a change of a flight directive; sensorially restoring the selected information. Various developments are described, notably links to documentary resources, the determination of anomalies, the use of predefined logic rules and configuration options. System aspects and software aspects are described.
摘要翻译：用于管理飞机飞行的计算机实施的方法包括以下步骤：接收与这些指令相关联的飞行指令和飞行信息; 确定飞机的飞行情况; 根据确定的上下文的功能，从与指令的制定和/或与当前航班指令和/或随着飞行指令的改变相关联的信息中选择信息; 感觉恢复所选信息。描述了各种发展，特别是与文献资源的链接，异常的确定，使用预定义的逻辑规则和配置选项。描述系统方面和软件方面。

9. 外观设计

USD752101S1 Display screen with an icon 有权
公开(公告)号：USD752101S1
公开(公告)日：2016-03-22
申请号：US29494798
申请日：2014-06-24
申请人： THALES Avionics SAS
设计人： Patrick Mazoyer , Sonia Vautier , Bertrand Caudron De Coquereaumont

10. 外观设计

USD751605S1 Display screen with an icon 有权
公开(公告)号：USD751605S1
公开(公告)日：2016-03-15
申请号：US29494796
申请日：2014-06-24
申请人： THALES Avionics SAS
设计人： Patrick Mazoyer , Sonia Vautier , Bertrand Caudron De Coquereaumont

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