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公开(公告)号：US10748432B2
公开(公告)日：2020-08-18
申请号：US14858751
申请日：2015-09-18
申请人： DASSAULT AVIATION
摘要： 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.
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公开(公告)号：US09567098B2
公开(公告)日：2017-02-14
申请号：US13851667
申请日：2013-03-27
申请人： DASSAULT AVIATION
发明人： Paul Kou , Jerome Barral , Cyril Saint-Requier , Eric Boulle
摘要： 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.
摘要翻译： 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。
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公开(公告)号：US09729226B2
公开(公告)日：2017-08-08
申请号：US14729818
申请日：2015-06-03
申请人： DASSAULT AVIATION
发明人： Jérôme Barral , Eric Boulle , Hervé Laverne
CPC分类号： H04B7/26 , G08G5/0013 , G08G5/0021 , G08G5/0039 , H04W4/14
摘要： 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.
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公开(公告)号：US10109202B2
公开(公告)日：2018-10-23
申请号：US15063444
申请日：2016-03-07
申请人： DASSAULT AVIATION
发明人： Eric Boulle , Jean-Philipe Roue
摘要： 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.
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