公开(公告)号：US20170183085A1

公开(公告)日：2017-06-29

申请号：US15385966

申请日：2016-12-21

Applicant: DASSAULT AVIATION

Inventor： Arnaud BRANTHOMME ,  Guy SCHALLER ,  Lorianne BOUTZEN

IPC: B64C17/10 ,  B64C13/16 ,  G06F3/14 ,  B64C13/04

CPC classification number: B64C17/10 ,  B64C13/042 ,  B64C13/16 ,  B64D37/00 ,  B64D43/00 ,  F02C9/26 ,  G06F3/14

Abstract: A system for controlling and monitoring pieces of equipment of an aircraft, each piece of equipment being able to be switched between two logic activation state values, comprising a man-machine interface, a module for configuration of a functional activation state of a function able to be performed on at least pieces of equipment of a system of the aircraft, the functional activation state being configurable between an active state and an inactive state, the configuration module being adapted for detecting an action of selection of a functional activation state of the function by an operator, and a control and monitoring module configured for determining a logic activation state of each of the pieces of equipment of the system, so that, when each of the pieces of equipment is in the determined logic activation state, the function is in the selected functional activation state.

公开(公告)号：US20160343261A1

公开(公告)日：2016-11-24

申请号：US15158807

申请日：2016-05-19

Applicant: DASSAULT AVIATION

Inventor： Arnaud BRANTHOMME ,  Igor FAIN ,  Patrick DARSES

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

CPC classification number: G08G5/0086 ,  B64D43/00 ,  G01C23/00 ,  G06T15/20 ,  G08G5/0047 ,  G08G5/0078 ,  G08G5/0091 ,  G09G5/377 ,  G09G2340/04 ,  G09G2354/00 ,  G09G2380/12

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.

Abstract translation: 提供了一种用于显示与飞机的飞行有关的信息的系统和相关的方法。 显示系统包括显示装置，人机接口，用于动态产生合成图像的模块，每个模块包括对环境的合成描述和表示轨迹的曲线，所述模块被配置为产生以中心为中心的第一合成图像 第一中心点，用于指示其显示，并且通过所述人机界面检测操作者修改所述中心点的动作。 生成模块还被配置为根据所述修改动作来确定不管所述修改动作是沿着所述曲线定位的第二中心点，以产生以所述第二中心点为中心的第二合成图像，以及 命令其显示。

公开(公告)号：US20160343260A1

公开(公告)日：2016-11-24

申请号：US15158802

申请日：2016-05-19

Applicant: DASSAULT AVIATION

Inventor： Arnaud BRANTHOMME ,  Igor FAIN ,  Patrick DARSES

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

CPC classification number: G08G5/0086 ,  B64D43/00 ,  G01C23/00 ,  G06T15/205 ,  G08G5/0047 ,  G08G5/0078 ,  G08G5/0091 ,  G09G5/377 ,  G09G2340/04 ,  G09G2380/12

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.

Abstract translation: 提供了一种用于显示与飞机的飞行有关的信息的系统和相关的方法。 显示系统包括动态合成图像生成模块，其被配置为根据第一类型的透视图像和根据第二类型的图像的图像之间或在根据第二类型的图像之间的图像之间或在根据第二类型的图像之间产生至少两个连续的过渡合成图像 分别根据第一类型的透视图和透视图的类型，并且在连续的过渡时刻命令其显示。 每个转换图像围绕中间的中心点居中，从位于距离中间中心点的中间观察距离的中间视点看，该中间观察距离分别是递增函数，递减函数，递减函数 在该图像显示时，从作为递减函数的中间开放角度看，分别显示该图像的过渡时刻的递增函数。

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：US20160300551A1

公开(公告)日：2016-10-13

申请号：US15092838

申请日：2016-04-07

Applicant: DASSAULT AVIATION

Inventor： Arnaud BRANTHOMME ,  Gilles CONSTANT

IPC: G09G5/36 ,  G06T13/80 ,  G06F3/0482 ,  G06F3/0485 ,  G06F3/0484

CPC classification number: G09G5/363 ,  G05B23/0216 ,  G06F3/0482 ,  G06F3/04847 ,  G06F3/04855 ,  G06Q10/06 ,  G06T13/80 ,  G09G2340/145 ,  G09G2354/00 ,  G09G2380/12

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.

Abstract translation: 提供了一种用于可视化具有若干替代序列和相关过程的飞行器程序的系统。 该系统在显示器上包括显示器和显示管理组件，使得可以在显示器上显示该过程的连续步骤。 所述显示管理组件能够在所述显示器上显示所述过程的活动序列的活动步骤，所述过程的活动序列中的活动步骤之前的至少一个先前步骤并且在几个步骤之间定义一个替换，以及 在该过程的该活动序列中的活动步骤之后的至少一个步骤，而不显示位于可以在活动步骤之前的任何步骤可访问的过程的非活动序列上的过程的步骤。