公开(公告)号：US20150365161A1

公开(公告)日：2015-12-17

申请号：US14729818

申请日：2015-06-03

Applicant: DASSAULT AVIATION

Inventor： Jérôme BARRAL ,  Eric BOULLE ,  Hervé LAVERNE

IPC: H04B7/26 ,  H04W4/14

CPC classification number: H04B7/26 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0039 ,  H04W4/14

Abstract: A communication system for an aircraft with an external assembly and related method are provided. The system includes a unit for receiving incoming text messages, received from the outside assembly, and sending outgoing text messages, sent to the outside assembly; a display screen and a display management station, the display management station being able to display, on the display screen, a synthesis window showing a series of incoming text messages and/or outgoing text messages, each text message containing operating information about the aircraft. The display management station is able to display, in the synthesis window, an execution status indicator for an action to be performed remaining to be executed, associated with the incoming text message and/or the outgoing text message, in addition to the operating information of the aircraft.

Abstract translation: 提供了一种具有外部组件和相关方法的飞机通信系统。 该系统包括用于接收从外部组件接收的传入文本消息并发送发送到外部组件的传出文本消息的单元; 显示屏幕和显示管理站，所述显示管理站能够在所述显示屏幕上显示示出一系列传入文本消息和/或传出文本消息的综合窗口，每个文本消息包含关于所述飞行器的操作信息。 显示管理站能够在综合窗口中显示与进入的文本消息和/或输出文本消息相关联的待执行剩余待执行的动作的执行状态指示符，除了操作信息 飞机。

公开(公告)号：US20140207314A1

公开(公告)日：2014-07-24

申请号：US13851667

申请日：2013-03-27

Applicant: DASSAULT AVIATION

Inventor： Paul KOU ,  Jerome BARRAL ,  Cyril SAINT-REQUIER ,  Eric BOULLE

IPC: B64D45/00

CPC classification number: B64D45/00 ,  B64D43/00 ,  G01C23/00

Abstract: The system includes additional display means including at least one additional screen and additional graphic interface handling means of the additional screen (able to display on the additional screen, a summary window depending on the operational state of the aircraft. The summary window comprises at least one first pictogram able to be displayed on a first display window of main display means of the aircraft without being displayed on the second window of the main display means, and at least one second pictogram intended to be displayed on the second display window of the main display means without being displayed on the first window of the main display means.

Abstract translation: 该系统包括附加显示装置，其包括附加屏幕的至少一个附加屏幕和附加图形界面处理装置（能够在附加屏幕上显示取决于飞行器的操作状态的汇总窗口），总结窗口包括至少一个 可以在主显示装置的第二窗口上显示的第一个象形图能够显示在主显示装置的主显示装置的第一显示窗口上，以及要显示在主显示器的第二显示窗口上的至少一个第二象形图 意味着不显示在主显示装置的第一窗口上。

公开(公告)号：US20160275800A1

公开(公告)日：2016-09-22

申请号：US15063444

申请日：2016-03-07

Applicant: DASSAULT AVIATION

Inventor： Eric BOULLE ,  Jean-Philipe ROUE

IPC: G08G5/00 ,  G08G5/02

CPC classification number: G08G5/0039 ,  G05D1/042 ,  G05D1/0623 ,  G05D1/063 ,  G05D1/0638 ,  G05D1/0653 ,  G05D1/0661 ,  G05D1/0676 ,  G05D1/101 ,  G08G5/0052 ,  G08G5/006 ,  G08G5/0065 ,  G08G5/025

Abstract: A method and system for determining in real time a vertical trajectory of an aircraft is provided. The method includes a step for providing an initial vertical trajectory comprising an initial phase for changing flight level according to a first slope, between a first point at a first altitude, and a second point at a second altitude, at least one step for modifying the vertical trajectory, comprising a phase for detecting a triggering element when the aircraft is at the first altitude, when said triggering element is detected, and a phase for determining a modified vertical trajectory, said modified vertical trajectory comprising a modified phase for changing flight level according to a second predefined slope, from a modified point at said first altitude, distinct from said first point, to said second altitude.

Abstract translation: 提供一种用于实时确定飞行器的垂直轨迹的方法和系统。 该方法包括提供初始垂直轨迹的步骤，该初始垂直轨迹包括用于根据在第一高度的第一点与第二高度处的第二点之间的第一斜率来改变飞行高度的初始相位，用于修改 垂直轨迹，包括当所述飞行器处于第一高度时检测触发元件的相位，当检测到所述触发元件时，以及用于确定修改的垂直轨迹的相位，所述修改的垂直轨迹包括用于根据 到第二预定斜率，从所述第一高度的修改点，不同于所述第一点到所述第二高度。

公开(公告)号：US20160086495A1

公开(公告)日：2016-03-24

申请号：US14858751

申请日：2015-09-18

Applicant: DASSAULT AVIATION

Inventor： Jérôme LAGARDE ,  Eric BOULLE ,  Marie-Gabrielle LAFOUCRIERE ,  Jérôme BARRAL

IPC: G08G5/00 ,  B64D45/00 ,  G01S13/95

Abstract: A piloting assistance system of a platform, and associated method are provided. The system includes a first detector for detecting a windshear able to generate a first alert that the platform is approaching a windshear zone; a second detector for detecting a windshear able to generate a second alert indicating the presence of the platform in the windshear zone; and a guider of the platform. The guider is able to automatically select a first guidance mode when a first alert is generated by the first detector, and to automatically select at least one second guidance mode different from the first guidance mode when a second alert is generated by the second detector. The system includes an information device able to display unified windshear alert information and/or unified information for implementation of a guidance mode, shared by the first alert and the second alert.

Abstract translation: 提供平台的驾驶辅助系统及相关方法。 该系统包括用于检测能够产生平台正在接近风切变区域的第一警报的风切变的第一检测器; 第二检测器，用于检测能够产生指示所述平台在所述风切变区域中的存在的第二警报的风切变; 和平台的指导者。 当由第一检测器产生第一警报时，导向器能够自动选择第一引导模式，并且当由第二检测器产生第二警报时，自动选择与第一引导模式不同的至少一个第二引导模式。 该系统包括能够显示统一的风切变警报信息的信息装置和/或用于实现由第一警报和第二警报共享的引导模式的统一信息。