公开(公告)号：US11286056B2

公开(公告)日：2022-03-29

申请号：US15371927

申请日：2016-12-07

Applicant: DASSAULT AVIATION

Inventor： Jean-François Saez ,  Stéphane Drinal

IPC: G06F3/048 ,  B64D43/00 ,  G08G5/00 ,  G01C23/00 ,  G06F3/04817 ,  G06F3/0482 ,  G06F3/04847 ,  G06F3/04883

Abstract: A system for displaying information relative to an aircraft flight and related method are provided. This system comprises a display device, and a module for managing the display on the display device, the management module being configured for controlling the display, on a window of the display device, of a timescale representative of a time period of the flight, and for controlling the display, facing the timescale, of pieces of information relative to a series of events intended to occur in a time window comprised in the time period. The module for managing the display is configured for determining a position in time of the time window comprised in the time period and a duration of the time window, and for controlling the display, along the timescale, of a marker representative of the position in time and of the duration of the time window.

公开(公告)号：US20210374101A1

公开(公告)日：2021-12-02

申请号：US17332319

申请日：2021-05-27

Applicant: DASSAULT AVIATION

Inventor： Benjamin BRIAND ,  Michaël OCIEPKA ,  Stéphane ARDOUIN ,  Vincent HUBERT ,  Nicolas LHOPITEAU

IPC: G06F16/178

Abstract: An aircraft computer file distribution system comprises a store (36) of aircraft computer files for loading into at least one aircraft device (12) that is onboard, mobile or replicated on the ground. The system includes a file manager (44), configured for identifying an aircraft configuration of the aircraft with which the aircraft device (12) is associated and a computer configuration of the aircraft device (12); defining, among the computer files in the computer file store (36), at least one computer file loadable into the aircraft device (12) according to the identified aircraft configuration and computer configuration; and activating a synchronization for remote distribution of at least one computer file to be loaded into the aircraft device (12) selected from the one or more computer files loadable into the aircraft device (12) based on the identified aircraft configuration and computer configuration.

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

IPC: G06T15/00 ,  G08G5/00 ,  G01C23/00 ,  B64D43/00 ,  G06T15/20 ,  G09G5/377

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.

公开(公告)号：US20200302805A1

公开(公告)日：2020-09-24

申请号：US16821779

申请日：2020-03-17

Applicant: DASSAULT AVIATION

Inventor： Cyrille GRIMALD ,  Benoit URIEN

IPC: G08G5/00 ,  G05D1/04 ,  B64D45/00 ,  G06F16/29

Abstract: Aircraft mission calculation system includes a first calculator configured to calculate a plurality of iso-displacement curves from a selected point, at a displacement range corresponding to several successive displacement increments of the aircraft from the selected point, the iso-displacement curves being obtained at the displacement range for a displacement of the aircraft to a given flight level from displacements of the aircraft at distinct flight altitude levels. The first calculator is configured to determine, based on iso-displacement curves up to the given flight level, obtained at distinct flight altitude levels, taken at the same displacement range of the aircraft, an extended iso-displacement curve at the given flight level maximizing the displacement of the aircraft from the geographical point of origin or minimizing the displacement of the aircraft toward the geographical destination point.

公开(公告)号：US10748432B2

公开(公告)日：2020-08-18

申请号：US14858751

申请日：2015-09-18

Applicant: DASSAULT AVIATION

Inventor： Jérôme Lagarde ,  Eric Boulle ,  Marie-Gabrielle Lafoucriere ,  Jérôme Barral

IPC: G06F19/00 ,  G08G5/00 ,  G01S13/95 ,  B64D45/00

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.

公开(公告)号：US20200017233A1

公开(公告)日：2020-01-16

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

IPC: B64D45/00 ,  G08G5/00

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.

公开(公告)号：US20190352008A1

公开(公告)日：2019-11-21

申请号：US16413768

申请日：2019-05-16

Applicant: DASSAULT AVIATION

Inventor： François-Xavier D'ARBONNEAU ,  Patrick DARSES ,  Bruno FERRY ,  François SALMON-LEGAGNEUR ,  Jean-Christophe DENJEAN

IPC: B64D11/00

Abstract: A device for waking up a crew member resting on an aircraft includes a processing unit configured to detect current development parameters of the aircraft and/or to detect a state of consciousness of at least one other active crewmember. The processing unit is also configured to activate an apparatus for waking up the resting crew member, when at least one predetermined condition for waking up the resting crew member on one or several current parameters of the aircraft and/or on a parameter representative of the state of consciousness of the at least one other active crew member is satisfied.

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.

公开(公告)号：US20190164440A1

公开(公告)日：2019-05-30

申请号：US16199045

申请日：2018-11-23

Applicant: DASSAULT AVIATION

Inventor： Benjamin BRIAND ,  Cédric CARLE ,  Stéphane DRINAL ,  Cyrille GRIMALD ,  Jean-François SAEZ ,  Cyril SAINT REQUIER ,  Jean-Baptiste VALLART

IPC: G08G5/00 ,  G01C23/00

Abstract: An aircraft mission computing system includes an aircraft mission path computing engine, and a mission deck comprising a display and a display management assembly configured for displaying, on the display, at least one button for defining an operational specification of the mission. The computing engine is configured to be activated after defining the choice of operational specification using the definition button to determine at least one possible path of the aircraft based on the or each choice of defined operational specification using the or each definition button. The display management assembly is configured to display, on the display, after the activation of the computing engine, at least one outcome indicator providing mission feasibility information while respecting the or each operational specification choice.

公开(公告)号：US10295396B2

公开(公告)日：2019-05-21

申请号：US14388778

申请日：2013-03-26

Applicant: DASSAULT AVIATION

Inventor： Sebastien Dupont De Dinechin

IPC: G01G19/07 ,  G01G19/414

Abstract: A method for determining an estimated mass of an aircraft is provided. This method includes determining a first mass of the aircraft, from characteristics of the aircraft determined before or after takeoff of the aircraft, determining, during the flight of the aircraft, a second mass of the aircraft, from a lift equation of the aircraft expressing the mass of the aircraft as a function of information representative of the load factor of the aircraft, of a lift coefficient of the aircraft, of speed information of the aircraft and of a static pressure of a mass of air passed through by the aircraft, determined from measurements by sensors of the aircraft during the flight of the aircraft, evaluating the estimated mass at said determination moment, as a function of said first and second masses.