公开(公告)号：US20150034767A1

公开(公告)日：2015-02-05

申请号：US14444068

申请日：2014-07-28

Applicant: Airbus Operations S.A.S.

Inventor： Guillaume Pirat

IPC: B64D15/04 ,  F16K31/12

CPC classification number: B64D15/04 ,  B64D2033/0233 ,  F02C7/047 ,  F16K31/12 ,  Y02T50/672

Abstract: A method of regulating the de-icing of a leading edge of an aircraft includes regulating the flow of air used for de-icing by at least a first regulator valve in accordance with two regulation levels, a first regulation level corresponding to the regulated position of the first regulator valve and a second regulation level corresponding to the fully open position of the first regulator valve. A de-icing device enables implementation of the regulation method.

Abstract translation: 一种调节飞行器前缘除冰的方法包括根据两个调节级别调节用于至少第一调节阀的除冰空气的流动，第一调节水平对应于调节位置 第一调节阀和第二调节水平对应于第一调节阀的完全打开位置。 除冰装置能够实现调节方法。

公开(公告)号：US20150032299A1

公开(公告)日：2015-01-29

申请号：US14339220

申请日：2014-07-23

Applicant: AIRBUS OPERATIONS (S.A.S.)

Inventor： Guilhem PUYOU ,  Victor GIBERT ,  Fabien PERRIN

IPC: G05D1/10 ,  B64C13/16

CPC classification number: B64C13/16 ,  G05D1/0676 ,  G08G5/025

Abstract: A system and method are disclosed for automatic landing of an aircraft on a landing runway, including an on-board video camera intended to take images of the ground, image processor to extract from these images visual features of the landing runway, guidance system determining guidance commands of the aircraft to bring it into a nominal approach plane and to align it with the axis of the landing runway, from the respective positions of the visual features of the landing runway, in at least one of the images, where the guidance commands are supplied to a flight control computer.

Abstract translation: 公开了一种用于飞机在着陆跑道上的自动着陆的系统和方法，包括用于拍摄地面图像的车载摄像机，图像处理器从这些图像中提取着陆跑道的视觉特征，指导系统确定指导 飞机的命令使其进入标称接近平面，并且在着陆跑道的视觉特征的相应位置上将其与着陆跑道的轴线对准在至少一个图像中，其中指导命令是 提供给飞行控制计算机。

公开(公告)号：US20140354039A1

公开(公告)日：2014-12-04

申请号：US14289236

申请日：2014-05-28

Applicant: Airbus Operations (S.A.S.)

Inventor： Christian DONADILLE

IPC: H02H9/02 ,  B64D45/00

CPC classification number: H02H9/025 ,  B64D45/00 ,  H02H3/025

Abstract: The subject matter disclosed herein relates to methods and devices for protecting a circuit against overcurrents. The device uses variable impedance properties of a semiconductor switch and includes closed-loop control for controlling the impedance of the switch as a function of the overcurrents to be corrected. The physical design stresses of an electrical circuit, linked to the protection against overcurrents, can therefore be limited.

Abstract translation: 本文公开的主题涉及用于保护电路免于过电流的方法和装置。 该器件使用半导体开关的可变阻抗特性，并且包括用于根据要校正的过电流来控制开关的阻抗的闭环控制。 因此，可以限制与防止过电流保护相关联的电路的物理设计应力。

公开(公告)号：US20140346280A1

公开(公告)日：2014-11-27

申请号：US14283290

申请日：2014-05-21

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Florian Constans ,  Josep Boada-Bauxell ,  Pierre Scacchi

IPC: B64C19/00 ,  B64D31/04

CPC classification number: B64C19/00 ,  B64C13/04 ,  B64C13/16 ,  B64D31/04 ,  B64D31/06

Abstract: A system for controlling an aircraft control parameter including a control interface including a mobile element configured to move on a travel, of which at least two portions are separated by a neutral position; a return element bringing the mobile element back to the neutral position when it is not actuated; and an interaction element, and a control unit configured to memorize an item of information corresponding to a first position of the mobile element at an instant of activation of the interaction element; and generate a setpoint of the aircraft control parameter, as a function of a control associated with the first position of the mobile element for which said information has been memorized; or a current position of the mobile element, when this current position is situated on the same portion of travel as the first position and is more remote than the latter from the neutral position.

Abstract translation: 一种用于控制飞行器控制参数的系统，其包括控制接口，所述控制接口包括被配置为在行程上移动的移动元件，其中至少两个部分被中立位置分隔; 返回元件，当移动元件未被启动时返回到中立位置; 以及控制单元，被配置为在所述交互元件的激活时刻存储对应于所述移动元件的第一位置的信息项; 并且根据与已经存储了所述信息的移动元件的第一位置相关联的控制来生成飞行器控制参数的设定点; 或当该当前位置位于与第一位置相同的行进部分上并且比中立位置更远离移动元件的当前位置时，移动元件的当前位置。

公开(公告)号：US20140230539A1

公开(公告)日：2014-08-21

申请号：US14184081

申请日：2014-02-19

Applicant: AIRBUS ,  AIRBUS OPERATIONS (S.A.S.)

Inventor： Catalin Perju ,  LAURENT DELESSARD ,  JEROME ROBILLARD

IPC: B64D43/02

CPC classification number: B64D43/02 ,  G01D5/342 ,  G01D5/3473 ,  G01P13/025

Abstract: The invention relates to an angle measurement probe on board an aircraft, which comprises a fin, which can move in rotation about an axis, at least one first optical encoder and one second optical encoder, each comprising at least one disk, each disk being fixed at right angles to the central axis and being provided with at least two circular tracks, each track being provided with alternate opaque and transparent zones, means for processing the output signal from each encoder.

Abstract translation: 本发明涉及一种飞机上的角度测量探针，其包括可围绕轴线旋转的翅片，至少一个第一光学编码器和一个第二光学编码器，每个包括至少一个盘，每个盘固定 与中心轴成直角并且设置有至少两个圆形轨道，每个轨道设置有替代的不透明区域和透明区域，用于处理来自每个编码器的输出信号的装置。

公开(公告)号：US20140209742A1

公开(公告)日：2014-07-31

申请号：US14227265

申请日：2014-03-27

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Bernard GUERING ,  Yves DURAND

IPC: H05K7/02 ,  B64D47/00

CPC classification number: H05K7/02 ,  B64D47/00 ,  H05K7/1439 ,  H05K7/1449

Abstract: An electrical core of an aircraft is provided. The electrical core includes at least one shelf on which is disposed at least one module containing components and comprising at least one input able to be linked to at least one power supply cable and at least one output able to be linked to at least one output cable. In the module, the output cable or cables travel under or in the shelf disposed under the module.

Abstract translation: 提供飞机的电芯。 电芯包括至少一个搁架，其上布置有至少一个包含部件的模块，并且包括至少一个能够连接到至少一个电源电缆的输入端和至少一个可连接到至少一个输出电缆 。 在模块中，输出电缆或电缆在设置在模块下方的架子下方或下方。

公开(公告)号：US20140180504A1

公开(公告)日：2014-06-26

申请号：US14103224

申请日：2013-12-11

Applicant: AIRBUS OPERATIONS (S.A.S)

Inventor： Marc FERVEL ,  Antoine MAUSSION ,  Arnaud LECANU ,  Sylvain SAUVANT

IPC: B64C19/00

CPC classification number: H04L49/351 ,  H04L12/6418 ,  H04L45/24 ,  H04L49/552

Abstract: The invention relates to an aircraft control system, situated in the avionics bay, including a computer, a remote equipment, such as an actuator of control surfaces, and an AFDX network. The computer includes a first module and a second module, respectively connected to a corresponding first module and a second module of the equipment, by a first and a second virtual link sharing a common path through the network, the first and second virtual links being segregated by a separate encoding at the applicative level. A replication and/or frame switching device is connected, on the one hand, to the common port and, on the other hand, to the ports of the first and second modules of the equipment.

Abstract translation: 本发明涉及一种位于航空电子设备舱中的飞行器控制系统，包括计算机，诸如控制面的致动器的远程设备和AFDX网络。 计算机包括分别通过共享通过网络的公共路径的第一和第二虚拟链路连接到设备的对应的第一模块和第二模块的第一模块和第二模块，第一和第二虚拟链路被分离 通过应用级别的单独编码。 一方面，复制和/或帧切换设备连接到公共端口，另一方面连接到设备的第一和第二模块的端口。

公开(公告)号：US20140136101A1

公开(公告)日：2014-05-15

申请号：US14068809

申请日：2013-10-31

Applicant: Airbus Operations (S.A.S.)

Inventor： Stephane BOSTETTER ,  Maxime WACHENHEIM ,  Boris KOZLOW

IPC: G08G5/00 ,  G01C21/20

CPC classification number: G08G5/0052 ,  G01C21/20 ,  G01C23/00 ,  G08G5/003

Abstract: Method and device for aiding the guidance of an aircraft having to comply with at least one time constraint. The device can determine and present on a screen of the flight deck an offset in distance (ΔD) between the aircraft (AC) and a reference aircraft (Aref) which is defined to fly along the flight plan (TV) at an optimal speed to comply with the time constraint.

Abstract translation: 用于帮助指导飞机必须符合至少一个时间约束的方法和装置。 该装置可以在飞行甲板的屏幕上确定飞行器（AC）与被定义为沿着飞行计划（TV）飞行的参考飞机（Aref）之间的距离偏差（＆Dgr; D） 速度要符合时间限制。

公开(公告)号：US20140110529A1

公开(公告)日：2014-04-24

申请号：US14062069

申请日：2013-10-24

Applicant: Airbus Operations (S.A.S.)

Inventor： Bernard Guering

IPC: B64C1/06

CPC classification number: B64C1/061 ,  B64C1/18 ,  Y10T29/49622

Abstract: Such a fuselage includes cross-members adapted for the formation of a floor, at least one of said cross-members including an upper part, a lower part, linkage for the lower part to the upper part, and at least one opening for the passage of systems which is delimited between the lower part and the upper part. The upper part of the cross-member is fastened to the fuselage and is dimensioned so as to bear the stresses to which said cross-member may be subjected when the aircraft remains on the ground. The lower part is fastened to the upper part so as to reinforce it such that when assembled, the upper part and the lower part are adapted to bear the stresses to which the cross-member may be subjected in flight conditions of the aircraft.

Abstract translation: 这样的机身包括适于形成地板的横向构件，所述横向构件中的至少一个包括上部，下部，用于下部至上部的连杆，以及用于通道的至少一个开口 在下部和上部之间界定的系统。 横梁的上部被固定在机身上，并且其尺寸设计成当飞机保持在地面上时承受所述横梁可能经受的应力。 下部固定到上部，以便加强它，使得当组装时，上部和下部适于承受跨部件在飞行器的飞行状态下可能受到的应力。

公开(公告)号：US20140102625A1

公开(公告)日：2014-04-17

申请号：US14048162

申请日：2013-10-08

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Denis De Mattia

IPC: B32B5/26

CPC classification number: B32B5/26 ,  B29C33/044 ,  B29C33/405 ,  B29C70/384 ,  B29K2105/0872

Abstract: A method for fibre placement with the aid of a roller is provided. The roller is able to pivot about a rotation axis and to lay a plurality of first pre-impregnated fibres on second pre-impregnated fibres of a laying surface by rolling over said laying surface. The first fibres being distributed along a lower generatrix of the roller and being in contact with an outer surface of said roller over a contact arc. The method includes cooling the first pre-impregnated fibres in contact with the roller so as to enable them to slide on the outer surface of the roller and heating the second pre-impregnated fibres of the laying surface that are located at the front of the roller so as to promote the adhesion of the first fibres to the second fibres of the laying surface.

Abstract translation: 提供了借助于辊子进行纤维放置的方法。 辊能够围绕旋转轴线枢转并且通过在所述铺设表面上滚动而将多个第一预浸渍纤维铺设在铺设表面的第二预浸渍纤维上。 第一纤维沿着辊的下母线分布并且在接触弧上与所述辊的外表面接触。 该方法包括冷却与辊接触的第一预浸渍纤维，以使它们能够在辊的外表面上滑动并且加热位于辊前部的铺设表面的第二预浸渍纤维 从而促进第一纤维与敷设表面的第二纤维的粘附。