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。

公开(公告)号：US09305457B2

公开(公告)日：2016-04-05

申请号：US14155194

申请日：2014-01-14

Applicant: DASSAULT AVIATION

Inventor： Arnaud Hennequin ,  Hugues Abrassart

IPC: H04W4/00 ,  G08C17/02 ,  H04B1/3822 ,  H04B7/185 ,  H04N21/214

CPC classification number: G08C17/02 ,  H04B1/3822 ,  H04B7/18506 ,  H04N21/214 ,  H04W4/80

Abstract: The system according to the invention comprises a mobile electronic device, at least one local base, arranged near a predefined location in the cabin, an assembly for pairing the mobile electronic device with the local base, and at least one piece of functional equipment for managing the cabin environment. The memory of the mobile electronic device stores at least one software application for controlling the functional equipment. The pairing system is capable of sending the mobile electronic device at least one location identification data of the local base during pairing between the mobile electronic device and the local base, the mobile electronic device being able to configure the control software application, based on the location identification data.

Abstract translation: 根据本发明的系统包括移动电子设备，布置在机舱内的预定位置附近的至少一个本地基座，用于将移动电子设备与本地基座配对的组件以及用于管理的至少一个功能设备 客舱环境。 移动电子设备的存储器存储用于控制功能设备的至少一个软件应用程序。 配对系统能够在移动电子设备和本地基站之间配对期间向移动电子设备发送本地基站的至少一个位置标识数据，移动电子设备能够基于位置来配置控制软件应用 识别数据。

公开(公告)号：US20160094674A1

公开(公告)日：2016-03-31

申请号：US14865922

申请日：2015-09-25

Applicant: DASSAULT AVIATION

Inventor： Adrien DRION ,  Arnaud HENNEQUIN

IPC: H04L29/08

CPC classification number: H04L67/2833 ,  G06F8/60 ,  H04B7/18506 ,  H04L67/04 ,  H04L67/18

Abstract: An infrastructure for hosting services in an aircraft, and related access method are provided. The infrastructure includes a plurality of onboard platforms, each platform corresponding to a functional domain of the aircraft and hosting at least one service able to be implemented in the aircraft in the functional domain in question; at least one onboard communicator communicating with a ground structure, connected to each onboard platform; and at least one access portal able to allow centralized access to services hosted by all of the onboard platforms corresponding to the different functional domains of the aircraft.

Abstract translation: 提供飞机托管服务的基础设施和相关的访问方法。 基础设施包括多个板载平台，每个平台对应于飞行器的功能域，并承载能够在所涉及的功能域中的飞机中实施的至少一个服务; 至少一个与地面结构通信的车载通信器，连接到每个车载平台; 以及至少一个访问门户，其能够允许对与飞机的不同功能域对应的所有板载平台所托管的服务的集中访问。

公开(公告)号：US09159239B2

公开(公告)日：2015-10-13

申请号：US14089535

申请日：2013-11-25

Applicant: DASSAULT AVIATION

Inventor： Nicolas Le Corre ,  Sébastien Lepage ,  Alain Boucher

IPC: G06F19/00 ,  G06G7/70 ,  G08G5/00 ,  G05D1/00 ,  G05D1/06 ,  G08G5/02

CPC classification number: G08G5/00 ,  G05D1/0083 ,  G05D1/0676 ,  G08G5/025

Abstract: The method according to the invention comprise the following steps, dynamic measurement of the current geographical position of the aircraft, and its current ground speed, calculation of a first length representative of a flight phase of the aircraft, and calculation of a second length representative of a ground phase of the aircraft, calculation of the position of the stop point based on the first length, the second length and the current geographical position. The calculation of the first length comprises a phase for dynamically estimating a distance traveled by the aircraft during at least part of a flare phase of the aircraft.

Abstract translation: 根据本发明的方法包括以下步骤：飞行器当前地理位置的动态测量及其当前地面速度，代表飞行器飞行阶段的第一长度的计算，以及代表飞行器的第二长度的计算 飞机的地面相位，基于第一长度，第二长度和当前地理位置计算停止点的位置。 第一长度的计算包括一个阶段，用于动态地估计飞机在至少部分飞机的火炬阶段期间行驶的距离。

公开(公告)号：US09151720B2

公开(公告)日：2015-10-06

申请号：US13691354

申请日：2012-11-30

Applicant: DASSAULT AVIATION

Inventor： Gerard Leflour

IPC: G01R27/32 ,  G01N22/00 ,  G01N22/02

CPC classification number: G01N22/00 ,  G01N22/02 ,  G01R27/32

Abstract: A device including a holder and a transmitter supported by the holder is provided. The transmitter is capable of transmitting an electromagnetic signal toward the surface any transmission frequency (Fe). The device also includes a receiver for receiving a signal reflected on the surface. The device also includes a guide assembly for guiding the movement of the holder to move the transmitter and the receiver across from the surface, tangentially relative to the surface. The device also includes an extraction unit for extracting, in the signal received by the receiver, a shifted frequency component of the transmission frequency resulting from a local impedance variation of the surface. The extraction unit produces an extracted signal representative of the state of the surface from the shifted frequency component.

Abstract translation: 提供了包括保持器和由保持器支撑的变送器的装置。 发射机能够向地面传输电磁信号任何传输频率（Fe）。 该装置还包括用于接收在表面上反射的信号的接收器。 该装置还包括引导组件，用于引导保持器的移动，以使发射器和接收器相对于表面相切地从表面移动。 该装置还包括提取单元，用于在由接收器接收的信号中提取由表面的局部阻抗变化产生的传输频率的移位频率分量。 提取单元从移位的频率分量产生表示表面状态的提取信号。