公开(公告)号：US09718559B2

公开(公告)日：2017-08-01

申请号：US14269504

申请日：2014-05-05

Applicant: DASSAULT AVIATION

Inventor： Sebastien Dupont De Dinechin ,  Fabrice Vallete

IPC: G01C21/00 ,  B64D45/00 ,  G06T19/00 ,  G06T13/00 ,  G06F3/147 ,  G09G5/14 ,  G01C23/00

CPC classification number: B64D45/00 ,  G01C23/00 ,  G06F3/147 ,  G06T13/00 ,  G06T19/006 ,  G09G5/14 ,  G09G2340/12 ,  G09G2340/125 ,  G09G2354/00 ,  G09G2358/00 ,  G09G2380/12

Abstract: A device is provided for assisting in the piloting of a vehicle, in particular an aircraft. The device includes a surface displaying images and a display management unit for images designed to be displayed on the display surface superimposed on a view of the outside landscape. The management unit is capable of commanding the display of piloting information images on the display surface. The management unit is capable of commanding the display, for at least one of the piloting information images, of an animation intended to attract a user's attention to that piloting information image, the animation comprising the display of an alert image and the shrinkage of the alert image.

公开(公告)号：US09714100B2

公开(公告)日：2017-07-25

申请号：US14316459

申请日：2014-06-26

Applicant: DASSAULT AVIATION

Inventor： Francois-Xavier D'Arbonneau

IPC: G01M17/00 ,  B64F5/00 ,  G01C5/00 ,  G01C5/06 ,  G01C21/16 ,  G01P5/14 ,  G01P7/00 ,  G01P21/02 ,  G05D1/04

CPC classification number: B64F5/60 ,  G01C5/005 ,  G01C5/06 ,  G01C21/165 ,  G01P5/14 ,  G01P7/00 ,  G01P21/025 ,  G05D1/042

Abstract: A method for detecting a failure of at least one sensor onboard an aircraft implementing a baro-inertial loop is provided. The method includes implementing a baro-inertial loop including obtaining a computed vertical speed, then a short-term baro-inertial altitude, based on a double integration of the measured vertical acceleration; and developing at least one intermediate loop parameter based on a deviation between the short-term baro-inertial altitude and the pressure altitude. The method also includes observing at least one failure detection parameter obtained from one of the intermediate parameters of the baro-inertial loop; and determining the presence of a failure on one of the sensors of the aircraft based on the value of the observed failure detection parameter.

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：US20170152058A1

公开(公告)日：2017-06-01

申请号：US15364925

申请日：2016-11-30

Applicant: DASSAULT AVIATION

Inventor： Olivier MORELLEC ,  Philippe VORMS ,  Maxime PHILBERT

IPC: B64D45/00 ,  G08B6/00 ,  B64D43/00

CPC classification number: B64D45/00 ,  B64D43/00 ,  G06F3/016 ,  G06F3/0362 ,  G06F3/0482 ,  G08B6/00

Abstract: An interface system between a user and a display device in the cockpit of an aircraft, related aircraft and method are provided. The system includes a rotary controller configured to control a target on the display device; a target manager, controlled by the rotary controller for moving the target on the display device during the rotation of the rotary controller and/or for interacting with a field targeted by the target during the rotation of the rotary controller; a haptic feedback generator on the rotary controller during its rotation. The haptic feedback generator is configured to generate at least two distinct haptic profiles on the rotary controller depending on distinct system states and/or distinct man-machine interface states of the aircraft.

公开(公告)号：US20170092223A1

公开(公告)日：2017-03-30

申请号：US15273587

申请日：2016-09-22

Applicant: DASSAULT AVIATION

Inventor： Igor FAIN ,  Patrice KURDIJIAN

IPC: G09G5/00 ,  G09B9/30 ,  G06T17/00 ,  G06T7/00 ,  G06T19/00 ,  G06F3/01

CPC classification number: G09G5/003 ,  G06F3/012 ,  G06F3/013 ,  G06T7/11 ,  G06T7/70 ,  G06T17/00 ,  G06T19/006 ,  G09B9/301 ,  G09B19/003

Abstract: A three-dimensional simulation system for generating a virtual environment involving a plurality of users and associated method are provided. The system includes a first sensor detecting a viewing direction of a first user, a computing unit configured to create a three-dimensional simulation of the virtual environment, based on data received from the at least one first sensor; for at least one second user, an immersive retrieval assembly for the virtual three-dimensional simulation created by the computing unit. The system includes, for the first user, a second sensor detecting the position of part of an actual limb of the first user. The computing unit is configured to create, in the virtual three-dimensional simulation, an avatar of the first user, comprising a virtual head and a virtual limb, reconstituted and oriented relative to one another based on data from the first sensor and the second sensor.

公开(公告)号：US09567098B2

公开(公告)日：2017-02-14

申请号：US13851667

申请日：2013-03-27

Applicant: DASSAULT AVIATION

Inventor： Paul Kou ,  Jerome Barral ,  Cyril Saint-Requier ,  Eric Boulle

IPC: B64D45/00 ,  G01C23/00 ,  B64D43/00

CPC classification number: B64D45/00 ,  B64D43/00 ,  G01C23/00

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20160379502A1

公开(公告)日：2016-12-29

申请号：US15189907

申请日：2016-06-22

Applicant: DASSAULT AVIATION

Inventor： Sébastien LEPAGE ,  Olivier BAUDSON ,  Arnaud TURPIN

IPC: G08G5/02 ,  G08G5/00 ,  B64D45/08

CPC classification number: G08G5/025 ,  B64D43/00 ,  B64D45/08 ,  G01C23/005 ,  G08G5/0021 ,  G08G5/0086

Abstract: A display system of an aircraft, including a flare guiding cue and related method are provided. The display system includes a display unit; and an assembly for generating a display on the display unit, configured to dynamically display, on the display unit, at least one horizon line, a slope scale of the aircraft relative to the horizon line, and a speed vector symbol, representative of the slope of the aircraft relative to the horizon line. The display generator is configured to display, upon approaching a landing strip, a flare guidance symbol, the position of the flare guidance symbol on the display unit depending on the topographical slope of the approached landing strip.

Abstract translation: 提供飞机的显示系统，包括火炬指导提示和相关方法。 显示系统包括显示单元; 以及用于在所述显示单元上生成显示器的组件，被配置为在所述显示单元上动态地显示所述飞机相对于所述水平线的至少一个水平线，斜率以及代表所述斜率的速度矢量符号 的飞机相对于地平线。 显示发生器被配置为在接近着陆条时，根据接近的着陆带的地形坡度，在展示单元上显示火炬引导符号的位置。

公开(公告)号：US20160376026A1

公开(公告)日：2016-12-29

申请号：US15189897

申请日：2016-06-22

Applicant: DASSAULT AVIATION

Inventor： Olivier BAUDSON ,  Arnaud TURPIN

IPC: B64D45/08 ,  G02B27/01 ,  B64D43/00 ,  G09G3/00

CPC classification number: B64D45/08 ,  B64D43/00 ,  G01C23/00 ,  G02B27/0101 ,  G02B27/0172 ,  G02B2027/014 ,  G02B2027/0141 ,  G08G5/0021 ,  G08G5/025 ,  G09G3/002 ,  G09G2380/12

Abstract: A display system of an aircraft, able to display a localization marking of a zone of location of an approach light ramp and related method are provided. The display system includes a display unit and an assembly generating a display on the display unit. The display generator is able to display, on approach to a landing strip, a localization marking of a presence zone of an approach light ramp toward the landing strip.

Abstract translation: 提供了能够显示进场光斜坡位置区域的定位标记和相关方法的飞机的显示系统。 显示系统包括显示单元和在显示单元上产生显示器的组件。 显示发生器能够在接近着陆带时显示朝向着陆带的接近光斜坡的存在区域的定位标记。

公开(公告)号：US20160340042A1

公开(公告)日：2016-11-24

申请号：US15160235

申请日：2016-05-20

Applicant: DASSAULT AVIATION

Inventor： Denis PEUZIAT

IPC: B64D11/00 ,  B64D11/06

CPC classification number: B64D11/00153 ,  B60R11/0235 ,  B60R2011/0082 ,  B64D11/0646 ,  F16M11/041 ,  F16M11/14 ,  F16M11/2071 ,  F16M11/24 ,  F16M13/02 ,  F16M2200/028 ,  F16M2200/068

Abstract: A retractable support for a screen, and aircraft cabin seat including such a support are provided. The retractable support for a screen comprises a support arm for the screen and a housing for receiving the arm in a retracted position inside the housing. The housing comprises a mechanism for deploying the arm outside the housing. The support further comprises a compartment defining a cavity for receiving the housing in a retracted position inside the compartment. The housing is mounted movably relative to the compartment between the retracted position and a free position outside the compartment.

Abstract translation: 提供了一种用于屏幕的伸缩支撑件，以及包括这种支撑件的飞机机舱座椅。 屏幕的可伸缩支撑件包括用于屏幕的支撑臂和用于将手臂接收在壳体内的缩回位置的壳体。 壳体包括用于将臂部分布置在壳体外部的机构。 支撑件还包括限定用于在壳体内的收缩位置中容纳壳体的腔室。 所述壳体相对于所述隔室可移动地安装在所述缩回位置和所述隔室外部的自由位置之间。

公开(公告)号：US09443435B2

公开(公告)日：2016-09-13

申请号：US14044305

申请日：2013-10-02

Applicant: DASSAULT AVIATION

Inventor： Olivier Baudson ,  Arnaud Turpin

IPC: G08G5/00 ,  G06T19/00

CPC classification number: G08G5/0047 ,  G01C23/00 ,  G06T19/006

Abstract: The system according to the invention comprises an assembly for managing the graphic interface of a display, capable of controlling the display, on at least a first region of the display, of a peripheral area formed by a synthetic image comprising at least one synthetic surface representation of the terrain, and capable of maintaining at least one area representative of the position of a landing runway, centered on the landing runway, and at least one front area, adjacent to the center area, substantially free of any synthetic surface representation of the terrain. The management assembly includes means for dynamically defining the length (L) of the front area on the display as a function of a vertical decision position (DP) associated with a selected approach for said landing runway.

Abstract translation: 根据本发明的系统包括用于管理显示器的图形界面的组件，其能够在显示器的至少第一区域上控制由包括至少一个合成表面表示的合成图像形成的外围区域的显示器 并且能够保持代表在着陆跑道上的着陆跑道的位置的至少一个区域，以及与中心区域相邻的至少一个前区域，基本上没有地形的任何合成表面表示 。 管理组件包括用于根据与所述着陆跑道的所选方法相关联的垂直决定位置（DP）来动态地定义显示器上的前区域的长度（L）的装置。