公开(公告)号：US10118703B2

公开(公告)日：2018-11-06

申请号：US15489680

申请日：2017-04-17

Applicant: DASSAULT AVIATION

Inventor： Michel Mihai ,  Gaëtan Lamothe

IPC: A47C4/00 ,  B64D11/06

Abstract: Armrest for aircraft seat, associated seat and process are provided. The armrest includes a stationary part (12) intended to be connected to the seat, a moving part (14) movable relative to the stationary part (12), between a high position in which the moving part (14) is intended to protrude above a seat bottom of the seat and a low position, and a maneuvering mechanism (18) able to guide the movement of the moving part (14) between the high position and the low position. The maneuvering mechanism (18) includes at least a first connecting rod (26) and a second connecting rod (27), each independently connecting the stationary part (12) to the moving part (14), the first connecting rod (26) and the second connecting rod (27) being arranged parallel to one another during the movement of the moving part (14) between the high position and the low position.

公开(公告)号：USD830949S1

公开(公告)日：2018-10-16

申请号：US29603981

申请日：2017-05-15

Applicant: DASSAULT AVIATION

Designer： Marion D'Halluin ,  Jean-Remi Billon ,  Matthieu Poidatz ,  Agnès Gervais ,  Maxime Robert

公开(公告)号：USD830284S1

公开(公告)日：2018-10-09

申请号：US29603985

申请日：2017-05-15

Applicant: DASSAULT AVIATION

Designer： Marion D'Halluin ,  Jean-Remi Billon ,  Matthieu Poidatz ,  Agnès Gervais ,  Maxime Robert

公开(公告)号：US10078100B2

公开(公告)日：2018-09-18

申请号：US14388781

申请日：2013-03-26

Applicant: DASSAULT AVIATION

Inventor： Sebastien Dupont De Dinechin

IPC: G06F19/00 ,  G01P21/00 ,  G01P13/02 ,  G01P5/16 ,  B64D43/02 ,  G01B21/00 ,  G01G23/01 ,  G01M9/06 ,  G01P3/80

CPC classification number: G01P21/00 ,  B64D43/02 ,  G01B21/00 ,  G01G23/01 ,  G01M9/06 ,  G01P3/806 ,  G01P5/16 ,  G01P13/025

Abstract: A method for determining a state of credibility of measurements made by sensors of an aircraft is provided. This method includes determining a speed of the aircraft, from static and total pressure measurements, determining a coefficient of lift of the aircraft from an incidence measurement and from said speed, determining a weight of the aircraft, determining if an equation of lift of the aircraft is satisfied, activating a state of optimal credibility, wherein the measurements made by said sensors are considered to be reliable if the said equation of lift is satisfied, activating a state of non-optimal credibility, wherein the measurements of at least one sensor are considered to be unreliable if the said equation of lift is not satisfied.

公开(公告)号：US10038985B2

公开(公告)日：2018-07-31

申请号：US15211528

申请日：2016-07-15

Applicant: DASSAULT AVIATION

Inventor： Stéphane Gouverneur

IPC: H04W84/04 ,  H04W88/02 ,  H04B7/185 ,  H04W4/04 ,  H04W76/15 ,  H04L29/12 ,  H04W76/02 ,  H04W84/06

CPC classification number: H04W4/42 ,  H04B7/185 ,  H04L61/605 ,  H04W4/40 ,  H04W76/15 ,  H04W84/06 ,  H04W88/02

Abstract: A communication method between an embedded communication system of an aircraft and a communication device is provided. The method includes a step for establishing a communication between the embedded communication system and the communication device, done according to a communication parameter associated with the communication device, contained in a memory of a communication terminal. The establishment step includes a phase for establishing a first auxiliary communication between terminal and the communication system, a phase for establishing a second auxiliary communication between the terminal and the communication device, according to the communication parameter, and a phase for transferring the second auxiliary communication from the terminal toward the communication system.

公开(公告)号：US20170313425A1

公开(公告)日：2017-11-02

申请号：US15497916

申请日：2017-04-26

Applicant: DASSAULT AVIATION

Inventor： Mathieu SENET

IPC: B64D11/00 ,  B64D45/00

CPC classification number: B64D11/0015 ,  B64D11/04 ,  B64D45/00 ,  B64D2045/007

Abstract: Avionics system for assisting implementation of security measures onboard an aircraft, aircraft comprising such a system, and associated method are provided. The avionics system is intended to assist the occupants of an aircraft in implementing security measures onboard the aircraft. It includes a parameter collector for collecting at least one avionics parameter of the aircraft, a context finder to determine a context from the or each avionics parameter collected by the collector, an instruction identifier to identify at least one relevant security instruction based on the context determined by the context finder, and at least one instruction submitter to submit the or each relevant security instruction to a passenger of the aircraft.

公开(公告)号：US20170297722A1

公开(公告)日：2017-10-19

申请号：US15489680

申请日：2017-04-17

Applicant: DASSAULT AVIATION

Inventor： Michel MIHAI ,  Gaëtan LAMOTHE

IPC: B64D11/06

CPC classification number: B64D11/0644 ,  B60N2/753

Abstract: Armrest for aircraft seat, associated seat and process are provided. The armrest includes a stationary part (12) intended to be connected to the seat, a moving part (14) movable relative to the stationary part (12), between a high position in which the moving part (14) is intended to protrude above a seat bottom of the seat and a low position, and a maneuvering mechanism (18) able to guide the movement of the moving part (14) between the high position and the low position. The maneuvering mechanism (18) includes at least a first connecting rod (26) and a second connecting rod (27), each independently connecting the stationary part (12) to the moving part (14), the first connecting rod (26) and the second connecting rod (27) being arranged parallel to one another during the movement of the moving part (14) between the high position and the low position.

公开(公告)号：US09487166B2

公开(公告)日：2016-11-08

申请号：US13871404

申请日：2013-04-26

Applicant: DASSAULT AVIATION

Inventor： Renaud Loison ,  Olivier Savin

IPC: B60R16/033 ,  H02J3/38 ,  H02J15/00

CPC classification number: B60R16/033 ,  B64D2221/00 ,  H02J3/387 ,  H02J15/00

Abstract: The system according to the invention comprises: an electrical network, and a regulating assembly. The regulating assembly includes a secondary electric power source, a conversion assembly for an additional electric power injected on the electrical network, the conversion assembly being able, in a first configuration, to consume the additional electric power present on the network to create a supply fluid of the secondary source. The assembly includes a reservoir for each supply fluid, to collect the supply fluid produced by the conversion assembly.

Abstract translation: 根据本发明的系统包括：电网和调节组件。 调节组件包括二次电源，用于在电网上注入的附加电力的转换组件，该转换组件能够在第一配置中消耗存在于网络上的附加电力以产生供应流体 的次要来源。 组件包括用于每个供应流体的储存器，以收集由转换组件产生的供应流体。

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。

公开(公告)号：US20160264256A1

公开(公告)日：2016-09-15

申请号：US15060815

申请日：2016-03-04

Applicant: DASSAULT AVIATION

Inventor： Bruno RAMIREZ ,  Gilles CONSTANT ,  Gaëtan BRAMOULLÉ

IPC: B64D45/00

CPC classification number: B64D45/00 ,  G05B23/0272

Abstract: An assistance system for the implementation of aircraft procedures comprising a chain of operations to carry out is provided. The system includes a procedure database receiving the specifications of a plurality of procedures to be performed and a display and/or validation module which is able to collect the specifications of the procedure, to display a piece of characteristic information at least one operation of the procedure on the basis of the collected specifications, and/or to receive validation of the performance of at least one operation of the procedure. The system includes a conflict determination module which is able to generate for at least one operation of the procedure, feasibility information for the operation of the procedure during the course of the procedure, depending on the current operating states of the functional systems of the aircraft.

Abstract translation: 提供了一套执行飞机程序的辅助系统，其中包括执行一连串的操作。 该系统包括接收要执行的多个过程的规范的过程数据库以及能够收集该过程的规范的显示和/或验证模块，以显示一条特征信息，该程序的至少一个操作 在收集的规范的基础上，和/或接受对程序的至少一个操作的执行的验证。 该系统包括冲突确定模块，该冲突确定模块能够根据飞行器的功能系统的当前操作状态，在程序过程中产生用于程序的至少一个操作的可操作性信息以用于程序的操作。