DISPLAY DEVICE COMPRISING A DISPLAY SCREEN WITH CONTROLLED TRANSPARENCY
    1.
    发明申请
    DISPLAY DEVICE COMPRISING A DISPLAY SCREEN WITH CONTROLLED TRANSPARENCY 审中-公开
    显示设备,包含具有受控透明度的显示屏幕

    公开(公告)号:US20150309309A1

    公开(公告)日:2015-10-29

    申请号:US14648598

    申请日:2013-11-28

    Applicant: THALES

    CPC classification number: G02B27/0101 G02B27/01 G02F1/1334 G03B21/10 G03B21/28

    Abstract: The general field of the invention is that of display devices comprising at least one image projector comprising an image generator, projecting optics and a display screen, the image of said image generator being projected by the projecting optics onto said display screen. The display device according to the invention comprises means allowing the degree of optical transmission and the degree of optical scattering of said display screen to be controlled so as to make it completely transparent or completely scattering, the image being projected only in the latter case.

    Abstract translation: 本发明的一般领域是包括至少一个包括图像发生器,投影光学元件和显示屏的图像投影仪的显示装置,所述图像发生器的图像由投影光学元件投影到所述显示屏上。 根据本发明的显示装置包括允许控制所述显示屏的光透射度和光散射度以使其完全透明或完全散射的装置,仅在后一种情况下投影图像。

    AVIONIC SYSTEM COMPRISING MEANS FOR DESIGNATING AND MARKING LAND
    2.
    发明申请
    AVIONIC SYSTEM COMPRISING MEANS FOR DESIGNATING AND MARKING LAND 审中-公开
    包含用于指定和标记土地的手段的航空系统

    公开(公告)号:US20170053453A1

    公开(公告)日:2017-02-23

    申请号:US15307804

    申请日:2015-04-27

    Applicant: THALES

    Abstract: The general field of the invention is that of avionics systems intended to be used on aircraft in flight above a terrain. The avionics system comprises a display system and a navigation system. The display system comprises a head support equipped with a display device capable of generating images overlaid on said terrain, and a system for detecting posture of said helmet. The display system according to the invention comprises means for displaying a marking symbol in the display device, said symbol determining a given direction. The navigation system comprises geolocation means for said aircraft, a database of cartographic data representative of said terrain and computation means making it possible to determine the location of the area of the terrain arranged at the intersection of said given direction with said terrain, and means for recording and processing said location in the navigation system.

    Abstract translation: 本发明的一般领域是旨在用于飞越地面以上的飞机的航空电子系统。 航空电子系统包括显示系统和导航系统。 该显示系统包括:头部支架,其具有能够产生覆盖在所述地形上的图像的显示装置,以及用于检测所述头盔的姿势的系统。 根据本发明的显示系统包括用于在显示设备中显示标记符号的装置,所述符号确定给定的方向。 导航系统包括用于所述飞行器的地理定位装置,代表所述地形的制图数据的数据库和计算装置,使得可以确定布置在所述给定方向与所述地形的交点处的地形区域的位置,以及用于 在导航系统中记录和处理所述位置。

    DISPLAY SYSTEM COMPRISING A SCREEN COMPRISING AN ARRAY OF DIFFRACTIVE PATTERNS
    4.
    发明申请
    DISPLAY SYSTEM COMPRISING A SCREEN COMPRISING AN ARRAY OF DIFFRACTIVE PATTERNS 有权
    包含包含差异图案阵列的画面的显示系统

    公开(公告)号:US20150160546A1

    公开(公告)日:2015-06-11

    申请号:US14567718

    申请日:2014-12-11

    Applicant: THALES

    Abstract: The general field of the invention is that of display systems comprising an image projector and an associated display screen, the said display system being designed to be used by an observer situated at a given location, the said display screen comprising two transparent and substantially parallel faces, the said display screen comprising, on at least one of its transparent faces, a plurality of regularly distributed light-scattering patterns. The image projector according to the invention illuminating the screen under a plurality of angles of incidence determined by the position and the size of the display screen, the said angles of incidence being centred on a mean angle of incidence, the scattering patterns comprise a diffractive structure in order to diffract the light rays having at least the mean angle of incidence in one or more directions corresponding to the said given location of the observer.

    Abstract translation: 本发明的一般领域是包括图像投影仪和相关联的显示屏幕的显示系统的所述显示系统,所述显示系统被设计为由位于给定位置的观察者使用,所述显示屏幕包括两个透明且基本平行的面 所述显示屏在其至少一个透明面上包括多个规则分布的光散射图案。 根据本发明的图像投影仪以由显示屏幕的位置和尺寸确定的多个入射角照亮屏幕,所述入射角以入射角为中心,散射图案包括衍射结构 以便在对应于观察者的所述给定位置的一个或多个方向衍射具有至少平均入射角的光线。

    Method for estimating an environmental footprint of a flight of an aircraft and associated electronic estimating system

    公开(公告)号:US20240386517A1

    公开(公告)日:2024-11-21

    申请号:US18688780

    申请日:2022-09-06

    Applicant: THALES

    Abstract: The present invention relates to a method for estimating an environmental footprint of a flight of an aircraft. The method is implemented by a decentralized electronic estimating system including at least a first entity, a second entity and a third entity, the second entity being distinct from the first entity and the third entity. The method includes receipt, by the second entity, from the first entity, at least one datum relative to the aircraft or its environment during the flight. The method also includes association, by the second entity, of a measurement uncertainty with each datum received by the second entity. The method further includes estimation, by the third entity, of an environmental indicator representative of the environmental footprint, on the basis of at least one datum and of the uncertainty associated with the at least one datum.

    METHOD FOR COMMUNICATION BETWEEN AN AIR TRAFFIC CONTROL SYSTEM AND A COMMUNICATION MODULE

    公开(公告)号:US20240304096A1

    公开(公告)日:2024-09-12

    申请号:US18286545

    申请日:2022-04-14

    Applicant: THALES

    CPC classification number: G08G5/0039 G08G5/0043 G08G5/006 G08G5/0091

    Abstract: A method for communication between an air traffic control system and a communication module, the communication method includes a step of determining environmental optimization time slots based on the air traffic absorption capacities of the various flight information regions, the environmental optimization time slots at least partially covering one or more flight information regions, each environmental optimization time slot having an associated efficiency level; a step of negotiation, between the pilot via the communication module and the air traffic control system, to negotiate changes to the flight plan on the basis of the environmental optimization time slots and the environmental optimization levels of the environmental optimization time slots.

    METHOD FOR CONTROLLING A ROBOT-AIRCRAFT AND CORRESPONDING CONTROL SYSTEM

    公开(公告)号:US20230205204A1

    公开(公告)日:2023-06-29

    申请号:US17923488

    申请日:2021-05-03

    Applicant: THALES

    CPC classification number: G05D1/0055 G05D1/0088 B64U10/00 B64U2201/10

    Abstract: Method for controlling an unmanned aircraft piloted by a fully autonomous control system including a first decision module and a simplex piloting control module including a high-performance controller, a high-safety controller and a second decision module, the high-performance and high-safety controllers determining piloting commands for the robot-aircraft, according to which: —as long as a set of conditions is verified, implementation by the first decision module of a nominal piloting mode with delivery to the output of the automatic control system of the piloting commands delivered to the output of the simplex piloting control module; —otherwise, switching to an emergency piloting mode, an emergency piloting command is delivered to the output of the automatic control system for execution by the robot-aircraft, the first decision module preventing the delivery to the output of the automatic control system of the piloting commands delivered to the output of the simplex module.

    HEAD-MOUNTED DISPLAY SYSTEM COMPRISING HEADING SELECTION MEANS AND ASSOCIATED SELECTION METHOD
    9.
    发明申请
    HEAD-MOUNTED DISPLAY SYSTEM COMPRISING HEADING SELECTION MEANS AND ASSOCIATED SELECTION METHOD 审中-公开
    包含头部选择手段和相关选择方法的头部安装显示系统

    公开(公告)号:US20170038833A1

    公开(公告)日:2017-02-09

    申请号:US15305651

    申请日:2015-04-27

    Applicant: THALES

    Abstract: The general field of the invention is that of head viewing systems for aircraft comprising a head support, a viewing device, a detection of posture of said head support, means for detecting the current heading of an aircraft and means for graphically generating said heading. The system according to the invention comprises means of control, display and selection of headings arranged so as: to display in response to a first command, a second so-called setpoint heading and a third heading termed a “support heading” corresponding to the direction of the head support in a terrestrial reference frame, said direction given by the information arising from the detection of posture of said head support and the means for detecting the current heading; to replace, in response to a second command, said second heading by said third heading, said third heading thus becoming the new heading setpoint.

    Abstract translation: 本发明涉及用于飞机的头戴显示系统的一般领域,包括头部支撑件,显示装置,用于检测头部支撑件的姿势的装置,用于检测飞机的当前航向(C1)的装置,以及装置 用于图形生成所述标题。 本发明的系统包括用于控制,显示和选择标题的装置,其布置成:响应于第一命令,所述装置显示称为标题设定值的第二标题(C2)和第三标题(C3), 被称为对应于地面参考帧中的头部支撑的方向的支撑标题,由检测到头部支撑件的姿势所产生的信息给出的所述方向以及用于检测当前航向的装置; 并且响应于第二命令,所述装置用第三标题替换第二标题,所述第三标题从而变为新的标题设置值。

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