公开(公告)号：US20160234309A1

公开(公告)日：2016-08-11

申请号：US15010668

申请日：2016-01-29

Applicant: DASSAULT AVIATION

Inventor： Hugues ABRASSART

IPC: H04L29/08 ,  G06F15/167

CPC classification number: H04L67/1097 ,  G06F15/167 ,  H04L67/1095 ,  H04W4/046

Abstract: A method for exchanging data between a storage system on the ground-based and an onboard storage system of an aircraft is provided. The method includes a first step for synchronization of a set of data contained in the ground-based storage system with a corresponding set of data of a storage memory of a data exchange device, through a communications network, a step for coupling the data exchange device to a local internal network of the aircraft connected to the storage system, and then a second step for synchronization of the set of data of the storage memory with a corresponding set of data of the onboard storage system, through the local internal network.

Abstract translation: 提供了一种用于在飞机的基于地面的存储系统和机载存储系统之间交换数据的方法。 该方法包括：第一步骤，用于通过通信网络将包含在地面存储系统中的一组数据与数据交换设备的存储存储器的相应数据集同步，用于将数据交换设备 连接到存储系统的飞行器的本地内部网络，然后通过本地内部网络，将存储存储器的一组数据与车载存储系统的相应的一组数据同步的第二步骤。

公开(公告)号：US20160221678A1

公开(公告)日：2016-08-04

申请号：US15010722

申请日：2016-01-29

Applicant: DASSAULT AVIATION

Inventor： Yann MAILLAUT

IPC: B64D11/06

CPC classification number: B64D11/0638 ,  B64D11/0605

Abstract: An interior layout assembly of an aircraft cabin, and related method are provided. The assembly includes a table, a console defining a receiving housing and a cover mounted on the console. The cover in the closed configuration and the console define a passage slot between them. The assembly also includes a flap closing off the passage slot, movable by the table from an active configuration closing the passage slot to a retracted configuration freeing the passage slot during the passage of the table from its retracted position to the deployed position.

Abstract translation: 提供飞机机舱的内部布局组件及相关方法。 该组件包括一个桌子，一个限定接收外壳的控制台和一个安装在控制台上的盖子。 封闭配置中的盖子和控制台在它们之间定义通道槽。 该组件还包括一封闭通道槽的挡板，其可通过将工作台从关闭通道槽的活动构件移动到在桌子从其缩回位置到展开位置通过期间释放通道槽的缩回构型而移动。

公开(公告)号：US20160221677A1

公开(公告)日：2016-08-04

申请号：US15010696

申请日：2016-01-29

Applicant: DASSAULT AVIATION

Inventor： Nicolas HANCE

IPC: B64D11/06

CPC classification number: B64D11/0605 ,  B64D11/0638

Abstract: A supporting device for an interior layout assembly of an aircraft cabin, a related assembly and method are provided. The device includes a stationary frame; a table that can be deployed relative to the frame between a retracted position and a horizontal deployed position; a mechanism for guiding the movement of the table relative to the frame between the retracted position and the deployed horizontal position. The guide mechanism defines at least one bearing point for the table during its passage from the retracted position to the deployed horizontal position, the bearing point having a globally invariable position relative to the frame, the table being configured to pivot on the bearing point while moving laterally away relative to the bearing point, by sliding on the bearing point, to the deployed position.

Abstract translation: 提供了一种用于飞机机舱的内部布置组件的支撑装置，相关组件和方法。 该装置包括固定框架; 可以在缩回位置和水平展开位置之间相对于框架部署的桌子; 用于在缩回位置和展开的水平位置之间引导桌子相对于框架的运动的机构。 引导机构在其从缩回位置到展开的水平位置的过程中定义了桌子的至少一个支承点，所述支承点相对于所述框架具有全局不变的位置，所述工作台构造成在移动时在所述支承点上枢转 通过在支承点上滑动到相对于支承点的横向远离到展开位置。

公开(公告)号：US20150329195A1

公开(公告)日：2015-11-19

申请号：US14711699

申请日：2015-05-13

Applicant: DASSAULT AVIATION

Inventor： Eugène WIELGOSZ

IPC: B64C1/14

CPC classification number: B64C1/1453 ,  F01D25/32 ,  Y10T137/0318 ,  Y10T137/6906

Abstract: A drain mast or discharging fluids from an aircraft and associated method are provided. This drain mast includes a fairing including a base including an upstream section intended to be attached on an outer surface of the aircraft and a downstream section. The drain mast also includes a discharge nozzle including a discharge end opening onto the outside of the fairing, the discharge nozzle protruding from the downstream section in a first direction with respect to the base, the base and the discharge nozzle defining a tubular through-cavity, extending from the upstream section as far as the discharge end. The fairing also includes a profiled section for guiding air, protruding from the downstream section, in a direction opposite to the first direction, and configured for orienting an incident mass of air on the profiled section towards the discharge end.

Abstract translation: 提供排水桅杆或从飞机排出流体和相关方法。 这种排水桅杆包括整流罩，其包括底座，其包括旨在附接在飞行器的外表面上的上游部分和下游部分。 排水桅杆还包括排出喷嘴，该喷嘴包括在整流罩的外侧上的排出端开口，排出喷嘴相对于底座在第一方向上从下游部分突出，基部和排出喷嘴限定管状通孔 ，从上游部分延伸到排放端。 整流罩还包括用于引导空气的成型部分，其从下游部分沿与第一方向相反的方向突出，并且构造成用于将异型件上的入射空气质量定向到排出端。

公开(公告)号：US20150006021A1

公开(公告)日：2015-01-01

申请号：US14316441

申请日：2014-06-26

Applicant: DASSAULT AVIATION

Inventor： Francois-Xavier D'ARBONNEAU ,  Olivier Breton

IPC: G07C5/08 ,  B64D45/00

CPC classification number: G07C5/0816 ,  B64D45/00 ,  G01P5/16 ,  G01P21/025

Abstract: A method for detecting a failure of at least one sensor onboard an aircraft implementing wind detection is provided. The method includes measuring an airspeed of the aircraft; measuring a geographical speed of the aircraft; determining an instantaneous wind vector, based on the measured airspeed and geographical speed; establishing an instantaneous wind variation vector, based on the determined instantaneous wind vector; projecting the instantaneous wind variation vector on the direction of the vector of an air or geographical speed of the aircraft; and determining the presence of a failure based on the obtained projection.

Abstract translation: 提供一种用于检测执行风检测的飞行器上的至少一个传感器的故障的方法。 该方法包括测量飞行器的空速; 测量飞机的地理速度; 基于测量的空速和地理速度确定瞬时风向量; 基于确定的瞬时风矢量建立瞬时风向量; 将瞬时风力变化矢量投影到飞行器的空气或地理速度的矢量的方向上; 以及基于所获得的投影来确定故障的存在。

公开(公告)号：US20150006020A1

公开(公告)日：2015-01-01

申请号：US14316459

申请日：2014-06-26

Applicant: DASSAULT AVIATION

Inventor： Francois-Xavier D'ARBONNEAU

IPC: B64F5/00

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.

Abstract translation: 提供了一种用于检测执行压力 - 惯性环路的飞行器上的至少一个传感器故障的方法。 该方法包括基于所测量的垂直加速度的双重积分来实现巴洛惯性循环，包括获得计算的垂直速度，然后是短期压力惯性高度; 并且基于短期压力 - 惯性高度和压力高度之间的偏差来开发至少一个中间回路参数。 该方法还包括观察从压力 - 惯性环路的一个中间参数获得的至少一个故障检测参数; 并且基于观察到的故障检测参数的值来确定飞机的一个传感器上的故障的存在。

公开(公告)号：US20140097973A1

公开(公告)日：2014-04-10

申请号：US14044305

申请日：2013-10-02

Applicant: DASSAULT AVIATION

Inventor： Olivier BAUDSON ,  Arnaud TURPIN

IPC: G08G5/00

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：US20140097295A1

公开(公告)日：2014-04-10

申请号：US14044110

申请日：2013-10-02

Applicant: DASSAULT AVIATION

Inventor： Fabien BOUFFANAIS ,  Benoit DE MAQUEVILLE ,  Olivier GAVOUYERE ,  Zdenek JOHAN

IPC: B64C1/14

CPC classification number: B64C1/1484 ,  B64C1/1492 ,  B64D47/08

Abstract: The nose section for a flying machine according to the invention comprises an enclosure delimiting a nose cone extending along a longitudinal axis (A-A′), the enclosure delimiting a window, and a glass closing the window extending transversely relative to the longitudinal axis (A-A′). The nose section includes an optical sensor, in particular a camera, positioned in the enclosure behind the glass. The enclosure defines a recess, the window covered by the glass being at least partially positioned in the recess.

Abstract translation: 根据本发明的用于飞行机器的鼻部部分包括限定沿着纵向轴线（AA'）延伸的鼻锥的外壳，限定窗口的外壳和关闭相对于纵向轴线（AA'）横向延伸的窗口的玻璃， ）。 鼻部包括位于玻璃后面的外壳中的光学传感器，特别是相机。 外壳限定凹部，由玻璃覆盖的窗口至少部分地定位在凹部中。

公开(公告)号：US20140002107A9

公开(公告)日：2014-01-02

申请号：US13691354

申请日：2012-11-30

Applicant: DASSAULT AVIATION

Inventor： Gerard Leflour

IPC: G01N22/00

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

Abstract: The device according to the invention comprises a holder and a transmitter supported by the holder, the transmitter being capable of transmitting an electromagnetic signal toward the surface any transmission frequency (Fe). It includes a receiver for receiving a signal reflected on the surface. The device comprises 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. It comprises 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: 根据本发明的装置包括保持器和由保持器支撑的发射器，所述发射器能够向所述表面传输电磁信号任何传输频率（Fe）。 它包括用于接收在表面上反射的信号的接收器。 该装置包括用于引导保持器的运动的引导组件，以使发射器和接收器相对于表面相对于表面移动。 它包括提取单元，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。

公开(公告)号：US12252236B2

公开(公告)日：2025-03-18

申请号：US17574677

申请日：2022-01-13

Applicant: DASSAULT AVIATION

Inventor： Jérôme Cappelle ,  François Pineau ,  William Faysse

IPC: B64C13/50 ,  B64D31/04 ,  B64D31/06

Abstract: A system for piloting an aircraft includes a throttle, a flight parameter sensor system, and an engine calculator controlling thrust parameters of an engine of the aircraft. The piloting system includes a flight control unit connected to the engine calculator, the sensors and the throttle. The flight control unit generates a thrust control vector from a flight control law and sends a digital signal including the generated thrust control vector to the engine calculator. The engine calculator controlling said thrust parameters of the engine depending on the generated thrust control vector received.