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1.发明授权公开(公告)号：US10339820B2
公开(公告)日：2019-07-02
申请号：US15158807
申请日：2016-05-19
Applicant: DASSAULT AVIATION
Inventor： Arnaud Branthomme , Igor Fain , Patrick Darses
Abstract: A system for displaying information related to a flight of an aircraft and an associated method are provided. The display system comprises a display device, a man-machine interface, a module for dynamically generating synthesis images, each comprising a synthetic depiction of the environment and a curve representative of a trajectory, said module being configured to generate a first synthesis image centered around a first central point of interest, to command the display thereof, and to detect an action to modify the central point of interest by an operator via said man-machine interface. The generating module is also configured to determine, as a function of said modification action, a second central point of interest, situated along said curve whatever said modification action is, to generate a second synthesis image centered around said second central point of interest, and to command the display thereof.
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公开(公告)号：US11225335B2
公开(公告)日：2022-01-18
申请号：US16508268
申请日：2019-07-10
Applicant: DASSAULT AVIATION
Inventor： Cyril Saint Requier , Gilles Constant , Guy Schaller , Arnaud Branthomme , Magali Thorel
Abstract: An aircraft operational state monitoring system is provided that includes a module for acquiring a logic state of a plurality of components of the aircraft, the components belonging to airplane systems. The aircraft operational state monitoring system includes a module for determining the operability status of a plurality of macroscopic functions of the aircraft, each macroscopic function being defined independently of the components and airplane systems necessary for the performance of the macroscopic function, the operability status being determined based on logic states of the plurality of components between an operational status and at least one nonoperational status. The aircraft operational state monitoring system includes a display and at least one graphic display management assembly on the display, configured for displaying, on the display, summary indicators of the operability status of the macroscopic functions of the aircraft.
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3.发明授权公开(公告)号：US10861342B2
公开(公告)日：2020-12-08
申请号：US15158802
申请日：2016-05-19
Applicant: DASSAULT AVIATION
Inventor： Arnaud Branthomme , Igor Fain , Patrick Darses
Abstract: A system for displaying information related to a flight of an aircraft and an associated method are provided. The display system comprises a dynamic synthesis image generating module, configured to generate at least two successive transition synthesis images between an image according to a first type of perspective and an image according to a second type of perspective, or between an image according to a second type of perspective and an image according to a first type of perspective, respectively, and to command the display thereof at successive transition moments. Each transition image is centered around an intermediate central point of interest, seen from an intermediate point of view situated at an intermediate observation distance from the intermediate central point of interest, which is an increasing function, a decreasing function, respectively, of the transition moment at which the image is displayed, and seen from an intermediate opening angle, which is a decreasing function, an increasing function, respectively, of the transition moment at which this image is displayed.
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4.发明授权公开(公告)号：US10467989B2
公开(公告)日：2019-11-05
申请号：US15092838
申请日：2016-04-07
Applicant: DASSAULT AVIATION
Inventor： Arnaud Branthomme , Gilles Constant
IPC: G09G5/36 , G06F3/0482 , G06F3/0484 , G06F3/0485 , G06T13/80
Abstract: A system for visualizing an aircraft procedure having several alternate sequences and related process are provided. The system includes a display and a display management assembly on the display, making it possible to display successive steps of the procedure on the display. The display management assembly able to display, on the display, an active step of an active sequence of the procedure, at least one prior step preceding the active step in the active sequence of the procedure and defining one alternative among several series of steps, and at least one step after the active step in this active sequence of the procedure, without displaying a step of the procedure situated on an inactive sequence of the procedure that may be accessible from any step before the active step.
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