公开(公告)号：US20190171337A1

公开(公告)日：2019-06-06

申请号：US16093577

申请日：2017-04-14

Applicant: THALES

Inventor： Jean-Cédric PERRIN ,  Fany BARAILLER ,  Yannick LE ROUX ,  Patrick CAZAUX

IPC: G06F3/0482 ,  G06F3/0484 ,  G08G5/00

Abstract: A method of displaying data for the management of the flight of an aircraft includes the steps consisting in receiving the selection of an object on a display screen present in the cockpit of the aircraft; determining one or more flight commands associated with the selected object; selecting at least one flight command from among the one or more determined flight commands; generating a display panel comprising a plurality of display tiles, one of the tiles displaying data associated with the selected object and another tile displaying the flight command selected. Developments describe the updating of the panel as a function of a revision of the flight plan, the displaying of attributes of a flight command, conditional display modifications, modalities of unfurling or of folding of the display tiles, the taking into account of the visual density of display, the use of display rules, in particular as a function of flight context.

公开(公告)号：US20210335136A1

公开(公告)日：2021-10-28

申请号：US17236672

申请日：2021-04-21

Applicant: THALES

Inventor： Chris DESEURE ,  Sébastien BOUSSIRON ,  Yannick LE ROUX

IPC: G08G5/00

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：US20140132555A1

公开(公告)日：2014-05-15

申请号：US14066622

申请日：2013-10-29

Applicant: Thales

Inventor： Loïc BECOUARN ,  Yannick LE ROUX ,  Sylvain HOURLIER ,  Alexandre ALAPETITE ,  Rune FOGH ,  Henning Boje ANDERSEN

IPC: G06F3/0488

CPC classification number: G06F3/0488 ,  G06F3/04817 ,  G06F3/04886 ,  G06F2203/04806 ,  G06F2203/04808

Abstract: The general field of the invention is that of methods providing a secure control for an appliance by means of a visualization device having a tactile surface capable of detecting several simultaneous touches. The method according to the invention comprises: A first step of displaying on the visualization device a first symbol representing the control in a locked state; A second step of displaying, after a first touch on the tactile surface, a second symbol representing an “unlocking” gesture; A third step of performing said “unlocking” gesture; A fourth step of validating the command by two simultaneous touches at the sites of the first and second symbols; A fifth step of changing the appearance of the first symbol representing the control to be activated in an unlocked and activated state.

Abstract translation: 本发明的一般领域是通过具有能够检测多个同时触摸的触觉表面的可视化装置为器具提供安全控制的方法。 根据本发明的方法包括：第一步骤，在可视化设备上显示表示处于锁定状态的控制的第一符号; 第二步骤，在触觉表面上的第一次触摸之后，显示表示“解锁”手势的第二符号; 执行所述“解锁”手势的第三步骤; 通过在第一和第二符号的位置处的两个同时触摸来验证命令的第四步骤; 第五步，将处于未激活状态的表示要激活的控制的第一符号的外观改变。

公开(公告)号：US20130231804A1

公开(公告)日：2013-09-05

申请号：US13783148

申请日：2013-03-01

Applicant: THALES

Inventor： Xavier SERVANTIE ,  Yannick LE ROUX

IPC: B64D45/00

CPC classification number: B64D45/00 ,  G01C23/005 ,  G01P1/08

Abstract: The general field of the invention is that of devices for display and control of setpoints for automatic piloting for aircraft, configured to display the setpoints of speed, heading, climb slope and altitude. The various setpoints are displayed in the form of a graphical representation comprising: wheels graduated in speed and in altitude indicating the aircraft setpoint values; a circular heading rose, graduated and centred on a first symbol representing the aircraft, the heading setpoint being indicated by a second symbol representing the heading to be followed by the aircraft and disposed around the perimeter of the heading rose; and a vertical sectional view comprising a graduated semicircle centred on a third symbol representing the aircraft, the slope setpoint being indicated by a fourth symbol representing the slope to be followed by the aircraft and disposed around the perimeter of the semicircle.

Abstract translation: 本发明的一般领域是用于显示和控制用于飞行器的自动驾驶的设定点的装置，被配置为显示速度，航向，爬坡和高度的设定点。 各种设定点以图形表示的形式显示，包括：轮速分级，高度指示飞机设定值; 圆形标题上升，以代表飞机的第一个符号为中心，标题设定点由表示飞机后跟的标题的第二个符号表示，并围绕标题的周边设置; 以及垂直剖面图，其包括以表示飞行器的第三符号为中心的刻度半圆，斜率设定点由表示飞机将遵循的斜坡的第四符号指示并且设置在半圆的周边周围。

公开(公告)号：US20240211313A1

公开(公告)日：2024-06-27

申请号：US18542715

申请日：2023-12-17

Applicant: THALES

Inventor： Sébastien RAZE ,  François COULMEAU ,  Bruno CAPELLE ,  Yannick LE ROUX ,  Pierre MARIANI

IPC: G06F9/50

CPC classification number: G06F9/5027

Abstract: An edge computation device on board an aircraft is configured for communicating with one or a plurality of onboard electronic devices having certified operation, and with at least one remote computation system. Same includes local computational resources, and is configured for implementing a management module for a plurality of software applications suitable for providing at least one control parameter and/or receiving at least one datum from at least one onboard electronic device, a module for activating the execution of at least one of the stored software applications, a management module for an execution stack, configured for determining, for each software application to be executed, an allocation of local computation resources and, where appropriate, for executing locally a first part of the application, and for requesting remote execution, by means of the remote computation system, of a second part of the application to be executed.

公开(公告)号：US20220396368A1

公开(公告)日：2022-12-15

申请号：US17744703

申请日：2022-05-15

Applicant: THALES

Inventor： Mathieu BESNARD ,  Philippe CONI ,  Sarah EGEA ,  Yannick LE ROUX

IPC: B64D43/00 ,  B60K35/00

Abstract: A system for remote interaction with a pointing means of an aircraft cockpit display system, equipped with HMIs, includes three layers: a lower layer configured so as to receive wired electric power supply and data exchange connections; an upper layer comprising a hand-rest knob, at least one physical interaction means configured so as to interact on the pointing means for pointing at the HMIs of the cockpit, and a module with a touch-sensitive flat surface configured so as to interact on the pointing device for pointing at the HMIs of the cockpit and arranged in the extension of the hand-rest knob; and an intermediate layer configured so as to make it possible to modify the position of the upper layer.

公开(公告)号：US20180060298A1

公开(公告)日：2018-03-01

申请号：US15684279

申请日：2017-08-23

Applicant: THALES

Inventor： Yannick LE ROUX ,  Alexiane BAILLY ,  Stéphanie LAFON ,  François MICHEL

IPC: G06F17/27 ,  G06F3/023 ,  G06F3/16 ,  G06F3/0484 ,  G06F3/0482

CPC classification number: G06F17/278 ,  B64D43/00 ,  G01C23/00 ,  G06F3/0233 ,  G06F3/0482 ,  G06F3/04842 ,  G06F3/04847 ,  G06F3/147 ,  G06F3/167 ,  G07C5/006 ,  G07C5/008 ,  G07C5/085 ,  G07C2205/02 ,  G08G5/0013 ,  G08G5/0021 ,  G09G2380/10 ,  G09G2380/12 ,  H04L67/12

Abstract: An avionics system comprises an analysis system for analysing the data input, arranged so as to ensure the following functionalities: recognition of the characteristics of each datum and creation of a raw alphanumeric datum; decomposition of the raw alphanumeric datum into numerical values and into referenced parameters or into unreferenced information or into unutilizable information; verification of the consistency of the information emanating from the raw alphanumeric datum; transformation of the raw alphanumeric datum into utilizable alphanumeric datum; the alphanumeric data being displayed in a data “cloud” on the viewing device, the data being able to be selected, modified or moved by the interaction means.

公开(公告)号：US20140033107A1

公开(公告)日：2014-01-30

申请号：US13949164

申请日：2013-07-23

Applicant: Thales

Inventor： Yannick LE ROUX

IPC: G06F3/0481

CPC classification number: G06F3/0481 ,  G01C23/00 ,  G08G5/0026

Abstract: The general field of the invention is that of methods for displaying the geographical situation of an aircraft in flight on a visual display device. The geographical situation comprises a cartographic representation of the terrain flown over by the aircraft. Said geographical situation comprises two main display modes, known as “Arc” and “Rose”. The switch from the first mode to the second mode is made at least by means of a first step of selecting a model representing the position of the aircraft at the current time and arranged in the first mode and a second step of moving said model towards the position occupied in the second mode. The movement of the model causes the movement of the cartographic representation of the terrain being flown over, the steps of selection and movement being accomplished using a human-machine interface, which can be a graphic cursor control device or a touch-sensitive interface.

Abstract translation: 本发明的一般领域是用于在视觉显示装置上显示飞行中的飞机的地理情况的方法。 地理情况包括飞机飞越的地形的制图。 所说的地理情况包括两种主要的显示模式，称为“弧”和“玫瑰”。 至少通过第一步骤进行从第一模式到第二模式的切换，第一步骤是选择表示当前时间的飞行器的位置并被布置在第一模式中的模型，以及第二步骤，将模型移动到 在第二模式中占用的位置。 模型的运动导致地形的地图表示的移动被移动，使用可以是图形光标控制装置或触敏界面的人机界面来完成选择和移动的步骤。

公开(公告)号：US20240412508A1

公开(公告)日：2024-12-12

申请号：US18735728

申请日：2024-06-06

Applicant: THALES

Inventor： Victor BAULIER ,  Bruno CAPELLE ,  Yannick LE ROUX ,  Baptiste IDIART

IPC: G06V20/17 ,  G06V10/25 ,  G06V10/764 ,  G06V10/82

Abstract: The present invention relates to an obstacle detection method implemented by an obstacle detection system on-board an aircraft, the aircraft including at least one on-board camera having an associated field of view configured to acquire full-field digital images. The method comprises the steps of: (a)—reception (50) of at least one full-field digital image captured by said at least one on-board camera, b)—determination (54) of a spatial position of a zone of interest of predetermined size in said full-field digital image, and extraction (56) of said zone of interest from said full-field digital image, c)—implementation of an obstacle detection module (58) on said extracted zone of interest, implementing a neural network previously trained to detect and classify obstacles in images having said predetermined size, each obstacle detected being located in said zone of interest.

公开(公告)号：US20240210918A1

公开(公告)日：2024-06-27

申请号：US18542743

申请日：2023-12-17

Applicant: THALES

Inventor： Sébastien RAZE ,  François COULMEAU ,  Bruno CAPELLE ,  Yannick LE ROUX ,  Pierre MARIANI

IPC: G05B19/4155

CPC classification number: G05B19/4155 ,  G05B2219/31112

Abstract: A supervision device configured for communicating with a computation device onboard an aircraft, wherein the onboard edge device is configured for executing software applications related with one or a plurality of onboard electronic devices with certified operation, the supervision device comprising a human-machine interface and being configured for receiving, from the edge computation device, observability signals comprising data relating to local computing resources of the onboard edge computation device and information relating to the execution of at least one of the software applications, the supervision device including at least one computing processor configured for computing a state of operation of the edge computation device and a state of execution of the at least one software application from the received observability signals and for displaying the state of operation and the state of execution on the human-machine interface.