会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 发明授权
    • Checking of a communication system for an aircraft under development
    • 检查正在开发的飞机的通信系统
    • US08583316B2
    • 2013-11-12
    • US13075510
    • 2011-03-30
    • Yves WeilerLaurent Coloma
    • Yves WeilerLaurent Coloma
    • G01M17/00G06F7/00G06F19/00
    • H04L43/00
    • The invention relates to a method and a device for checking a communication system (3) comprising a plurality of modules (7) adapted to be installed in an aircraft under development (5), said checking device including: means (11) for building an identification and synchronization database (17) for said communication system (3), said database contractually defining interfaces between said plurality of modules from change notes relative to an initial technical definition, means (11) for defining, in said database (17), signals configured to be exchanged between said plurality of modules (7) via a plurality of connections (3) interconnecting said interfaces, said signals being defined to be synchronized with each other as well as with the physical materialization of said connections, and means (11) for checking, before an evaluation of a maturation test of the communication system (3), an interface consistency for all of said signals of said database (17).
    • 本发明涉及一种用于检查通信系统(3)的方法和装置,包括适于安装在正在开发的飞行器(5)中的多个模块(7),所述检查装置包括:用于构建 用于所述通信系统(3)的识别和同步数据库(17),所述数据库从相对于初始技术定义的变化说明书合同地定义所述多个模块之间的接口,用于在所述数据库(17)中定义信号 被配置为经由互连所述接口的多个连接(3)在所述多个模块(7)之间交换,所述信号被定义为彼此同步以及所述连接的物理实现,以及装置(11) 用于在所述通信系统(3)的成熟测试的评估之前检查所述数据库(17)的所有所述信号的接口一致性。
    • 2. 发明申请
    • CHECKING OF A COMMUNICATION SYSTEM FOR AN AIRCRAFT UNDER DEVELOPMENT
    • 检查发展飞机的通信系统
    • US20110270806A1
    • 2011-11-03
    • US13075510
    • 2011-03-30
    • Yves WeilerLaurent Coloma
    • Yves WeilerLaurent Coloma
    • G06F17/30
    • H04L43/00
    • The invention relates to a method and a device for checking a communication system (3) comprising a plurality of modules (7) adapted to be installed in an aircraft under development (5), said checking device including: means (11) for building an identification and synchronization database (17) for said communication system (3), said database contractually defining interfaces between said plurality of modules from change notes relative to an initial technical definition, means (11) for defining, in said database (17), signals configured to be exchanged between said plurality of modules (7) via a plurality of connections (3) interconnecting said interfaces, said signals being defined to be synchronized with each other as well as with the physical materialization of said connections, and means (11) for checking, before an evaluation of a maturation test of the communication system (3), an interface consistency for all of said signals of said database (17).
    • 本发明涉及一种用于检查通信系统(3)的方法和装置,包括适于安装在正在开发的飞行器(5)中的多个模块(7),所述检查装置包括:用于构建 用于所述通信系统(3)的识别和同步数据库(17),所述数据库从相对于初始技术定义的变化说明书合同地定义所述多个模块之间的接口,用于在所述数据库(17)中定义信号 被配置为经由互连所述接口的多个连接(3)在所述多个模块(7)之间交换,所述信号被定义为彼此同步以及所述连接的物理实现,以及装置(11) 用于在所述通信系统(3)的成熟测试的评估之前检查所述数据库(17)的所有所述信号的接口一致性。
    • 3. 发明申请
    • METHOD OF REGULATING A HARMONIZATION COMPENSATION BETWEEN VIDEO SENSOR AND HEAD UP DISPLAY DEVICE, AND CORRESPONDING DEVICES
    • 视频传感器与头戴式显示设备之间的协调补偿调节方法及相关设备
    • US20100060730A1
    • 2010-03-11
    • US12540605
    • 2009-08-13
    • Sandra POUSSINDavid BideauLaurent ColomaStephane Gauthier
    • Sandra POUSSINDavid BideauLaurent ColomaStephane Gauthier
    • H04N7/18
    • G02B27/01G02B2027/014
    • The invention relates to a method for adjustment of a harmonization compensation applied to alleviate a discrepancy of conformity between a video image transmitted by a video transducer (1) and projected by a head-up display device (5, 6), of an aircraft, and an external scene ahead of the aircraft. At least one equipment item of the aircraft—preferably the said HUD device—equipped with at least one control element accessible in the cockpit, is programmed to be able to function according to a nominal mode and according to a maintenance mode, in which at least one of its control elements, known as a redirected control element, is used to define the applied harmonization compensation. An operator activates the maintenance mode and starts an adjustment operation, in which he modifies in real time the applied harmonization compensation, by manipulating at least one redirected control element, until the video image is matched with the external scene.
    • 本发明涉及一种用于调整用于减轻由视频传感器(1)传输的视频图像并由飞机的平视显示设备(5,6)投影的视频图像之间的一致性差异)的调谐补偿的方法, 和飞机前的外部场景。 飞机的至少一个设备项目 - 优选地,所述HUD设备 - 配备有在驾驶舱中可访问的至少一个控制元件被编程为能够根据标称模式并且根据维护模式来运行,其中至少 被称为重定向控制元件的控制元件之一被用于定义所应用的协调补偿。 操作员激活维护模式并开始调整操作,其中他通过操纵至少一个重定向的控制元件实时修改应用的协调补偿,直到视频图像与外部场景匹配。
    • 4. 发明申请
    • CROSSED MONITORING DEVICE FOR HEAD-UP DISPLAYS
    • 用于头戴式显示器的交叉监视装置
    • US20100207843A1
    • 2010-08-19
    • US12682046
    • 2008-09-26
    • Laurent ColomaDavid Bideau
    • Laurent ColomaDavid Bideau
    • G09G5/12
    • G02B27/01G02B2027/0123G02B2027/014
    • A crossed monitoring device for a head-up display that can be used for displaying a representation of at least one first datum. The device includes a mechanism generating at least one first image from the at least one first datum, a mechanism receiving from the at least one second display at least one second image generated from at least one second datum, and a mechanism selecting one of the first and at least one second image. The device can further include a mechanism modifying images according to characteristics of the displays. Each display can modify the images to be displayed according to its characteristics, and each display can modify the images according to the characteristics of each display.
    • 用于平视显示器的交叉监视装置,其可用于显示至少一个第一数据的表示。 所述装置包括从所述至少一个第一基准产生至少一个第一图像的机构,从所述至少一个第二显示器接收从至少一个第二基准产生的至少一个第二图像的机构,以及选择所述第一数据中的一个的机构 和至少一个第二图像。 该装置还可以包括根据显示器的特征修改图像的机构。 每个显示器可以根据其特征修改要显示的图像,并且每个显示器可以根据每个显示器的特性来修改图像。
    • 5. 发明授权
    • Method of regulating a harmonization compensation between video sensor and head up display device, and corresponding devices
    • 调节视频传感器与抬头显示装置之间的协调补偿的方法及相应的装置
    • US08537214B2
    • 2013-09-17
    • US12540605
    • 2009-08-13
    • Sandra PoussinDavid BideauLaurent ColomaStephane Gauthier
    • Sandra PoussinDavid BideauLaurent ColomaStephane Gauthier
    • H04N7/00
    • G02B27/01G02B2027/014
    • The invention relates to a method for adjustment of a harmonization compensation applied to alleviate a discrepancy of conformity between a video image transmitted by a video transducer (1) and projected by a head-up display device (5, 6), of an aircraft, and an external scene ahead of the aircraft. At least one equipment item of the aircraft—preferably the said HUD device—equipped with at least one control element accessible in the cockpit, is programmed to be able to function according to a nominal mode and according to a maintenance mode, in which at least one of its control elements, known as a redirected control element, is used to define the applied harmonization compensation. An operator activates the maintenance mode and starts an adjustment operation, in which he modifies in real time the applied harmonization compensation, by manipulating at least one redirected control element, until the video image is matched with the external scene.
    • 本发明涉及一种用于调整用于减轻由视频传感器(1)传输的视频图像并由飞机的平视显示设备(5,6)投影的视频图像之间的一致性差异)的调谐补偿的方法, 和飞机前的外部场景。 飞机的至少一个设备项目 - 优选地,所述HUD设备 - 配备有在驾驶舱中可访问的至少一个控制元件被编程为能够根据标称模式并且根据维护模式来运行,其中至少 被称为重定向控制元件的控制元件之一被用于定义所应用的协调补偿。 操作员激活维护模式并开始调整操作,其中他通过操纵至少一个重定向的控制元件实时修改应用的协调补偿,直到视频图像与外部场景匹配。
    • 6. 发明授权
    • Crossed monitoring device for head-up displays
    • 用于平视显示器的交叉监视设备
    • US08497816B2
    • 2013-07-30
    • US12682046
    • 2008-09-26
    • Laurent ColomaDavid Bideau
    • Laurent ColomaDavid Bideau
    • G09G5/00
    • G02B27/01G02B2027/0123G02B2027/014
    • A crossed monitoring device for a head-up display that can be used for displaying a representation of at least one first datum. The device includes a mechanism generating at least one first image from the at least one first datum, a mechanism receiving from the at least one second display at least one second image generated from at least one second datum, and a mechanism selecting one of the first and at least one second image. The device can further include a mechanism modifying images according to characteristics of the displays. Each display can modify the images to be displayed according to its characteristics, and each display can modify the images according to the characteristics of each display.
    • 用于平视显示器的交叉监视装置,其可用于显示至少一个第一数据的表示。 所述装置包括从所述至少一个第一基准产生至少一个第一图像的机构,从所述至少一个第二显示器接收从至少一个第二基准产生的至少一个第二图像的机构,以及选择所述第一数据中的一个的机构 和至少一个第二图像。 该装置还可以包括根据显示器的特征修改图像的机构。 每个显示器可以根据其特征修改要显示的图像,并且每个显示器可以根据每个显示器的特性来修改图像。
    • 8. 发明申请
    • Set of equipment for an aircraft comprising a video sensor and at least two head-up display devices
    • 一套用于飞机的设备,包括视频传感器和至少两个平视显示设备
    • US20100265162A1
    • 2010-10-21
    • US12706352
    • 2010-02-16
    • Sandra PoussinDavid BideauLaurent ColomaStéphane Gauthier
    • Sandra PoussinDavid BideauLaurent ColomaStéphane Gauthier
    • G09G5/00
    • G02B27/01G02B2027/0138G02B2027/014
    • The invention relates to a set of equipment items for an aircraft comprising a video transducer (1) and at least two head-up display devices (2, 3), characterized in that the video transducer (1) and/or each HUD device (2, 3) is/are capable of defining the image to be projected by the said HUD device on the basis of the display field of the said HUD device and of one or more HUD/transducer errors, each HUD/transducer error being defined as being the difference between the HUD error of the corresponding HUD support around a direction and the transducer error around this same direction, the HUD error of an HUD support around a direction being the angular difference around this direction between the line of sight of the said HUD support and a measuring reference line, and the transducer error around a direction being the angular difference around this direction between the line of sight of the transducer support and a measuring reference line.
    • 本发明涉及一种用于飞行器的设备项目,其包括视频换能器(1)和至少两个平视显示设备(2,3),其特征在于,视频换能器(1)和/或每个HUD设备 2,3)能够基于所述HUD设备的显示区域和一个或多个HUD /换能器错误来定义由所述HUD设备投影的图像,每个HUD /换能器误差被定义为 作为相对于方向上的对应HUD支持的HUD误差与在该相同方向周围的换能器误差之间的差异,HUD支持的HUD误差围绕该方向在该方向之间的角度差在所述HUD的视线之间 支撑和测量参考线,以及围绕传感器支撑的视线与测量参考线之间的该方向周围的角度差的方向的换能器误差。