公开(公告)号：US10036651B2

公开(公告)日：2018-07-31

申请号：US15176682

申请日：2016-06-08

Applicant: THALES

Inventor： Sylvain Lissajoux ,  Bruno Aymeric ,  Didier Poisson

IPC: B64D43/02 ,  G01C23/00

CPC classification number: G01C23/005 ,  B64D43/02

Abstract: This electronic device for aiding with the piloting of an aircraft includes: an acquisition module, configured to acquire a current value of the roll angle of the aircraft; a computing module configured to compute a roll angle limit corresponding to a beginning of stalling of the aircraft; and a display module, configured to display, on a screen, a first symbol indicating a current orientation of the aircraft. The computing module is configured to compute at least one roll margin, each roll margin depending on a corresponding roll angle limit and the current value of the roll angle, and the display module is configured, when the display condition is verified, to display, on the screen, at least one second symbol positioned relative to the first symbol, the deviation between each second symbol and the first symbol representing a respective roll margin.

公开(公告)号：US09530321B2

公开(公告)日：2016-12-27

申请号：US14627645

申请日：2015-02-20

Applicant: THALES

Inventor： Guy Deker ,  Michel Roger ,  Bruno Aymeric

IPC: G01C23/00 ,  G08G5/00 ,  G05D1/10

CPC classification number: G08G5/0039 ,  G05D1/101 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0047 ,  G08G5/0052 ,  G08G5/0095

Abstract: A method and system, for flight management of an aircraft flying on a trajectory shifted with respect to a flight plan comprising a plurality of constrained waypoints, comprises a step of determining and displaying at least one point of the trajectory, termed decision point, beyond which the aircraft can no longer rejoin a constrained waypoint of the flight plan by determining a point of intersection between the trajectory and a rejoining trajectory steering towards the selected constrained waypoint, the rejoining trajectory complying with at least one predefined criterion.

公开(公告)号：US09520065B2

公开(公告)日：2016-12-13

申请号：US14492864

申请日：2014-09-22

Applicant: THALES

Inventor： Bruno Aymeric ,  Xavier Servantie ,  Cécile Andre

IPC: G01C5/00 ,  G01C23/00 ,  G01D7/04 ,  G08G5/00

CPC classification number: G08G5/0047 ,  G01C5/005 ,  G01C23/00 ,  G01D7/04

Abstract: A navigation aid information display device of an aircraft and primary flight display for an aircraft are disclosed. In one aspect, the navigation aid information display system includes a display screen including at least one first display area configured to display a first altitude scale including graduations, the current altitude of the aircraft on the first scale, and set altitude value. The graduations of the first scale are distributed on an arc of a first disc including a first needle centered in the disc and the first needle is configured to indicate the current altitude on the first scale. The distribution of the graduations on the arc is nonlinear and symmetrical relative to a graduation corresponding to the set altitude value and defines extension graduations decreasing from the set altitude value.

Abstract translation: 公开了飞机的导航辅助信息显示装置和飞行器的主飞行显示器。 一方面，导航辅助信息显示系统包括显示屏幕，其包括被配置为显示包括刻度的第一高度刻度，第一刻度上的飞行器的当前高度和设置的高度值的至少一个第一显示区域。 第一刻度的刻度分布在包括在盘中心的第一针的第一盘的圆弧上，并且第一针被配置为指示第一刻度上的当前高度。 圆弧上的刻度分布相对于与设定的高度值相对应的刻度是非线性的和对称的，并且定义从设定的高度值减小的延伸刻度。

公开(公告)号：US09202381B2

公开(公告)日：2015-12-01

申请号：US14069272

申请日：2013-10-31

Applicant: THALES

Inventor： Bruno Aymeric ,  Cécile Andre ,  Yannick Le Roux ,  François Michel

IPC: G01C23/00 ,  G08G5/00

CPC classification number: G08G5/003 ,  G01C23/00 ,  G08G5/0021 ,  G08G5/0034 ,  G08G5/0039

Abstract: The general field of the invention is that of methods of graphic representation, modification and validation of an aeronautical flight plan for an aircraft avionics system. The system comprises means for computing and generating said flight plan, a task management system, a visualization device displaying a graphic representation of said flight plan and a man-machine interface suitable for making selections, modifications or additions to the information contained in said graphic representation, said selections, modifications and additions being taken into account by the task management system, said graphic representation containing a timeline on which feature at least the various phases of the flight plan and the information corresponding to said phases. The method according to the invention contains a step of displaying at least one item of information depending on several parameters and the graphic representation of which depends on the level of available information about said parameters.

Abstract translation: 本发明的一般领域是用于飞机航空电子系统的航空飞行计划的图形表示，修改和验证的方法。 该系统包括用于计算和产生所述飞行计划的装置，任务管理系统，显示所述飞行计划的图形表示的可视化装置以及适于对包含在所述图形表示中的信息进行选择，修改或添加的人机界面 ，所述选择，修改和添加被所述任务管理系统考虑在内，所述图形表示包含至少在飞行计划的各个阶段的特征以及对应于所述阶段的信息的时间线。 根据本发明的方法包括根据几个参数显示至少一个信息项的步骤，并且其图形表示取决于关于所述参数的可用信息的级别。