公开(公告)号：US20170352204A1

公开(公告)日：2017-12-07

申请号：US15606917

申请日：2017-05-26

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

Inventor： Jean-Max HUET ,  Franck DULUC ,  Eric BENHAMOU ,  Bruno MAILLARD

IPC: G07C5/08 ,  B64D45/00 ,  G06N5/04 ,  G06N99/00

CPC classification number: G07C5/0808 ,  B64D45/00 ,  G05B23/0221 ,  G06F11/008 ,  G06N5/04 ,  G06N20/00

Abstract: The disclosure herein proposes identifying precursors to all the phenomena which can have an impact on the service use of an aircraft. It relates to a system for predicting failures in an aircraft, including a processor configured to analyze a current behavior of at least one flight parameter of the aircraft to detect any deviation of the current behavior relative to a predetermined behavior model of the parameter, the behavior model being determined from a plurality of series of learning data relating to the parameter collected during the flights of a set of aircraft.

公开(公告)号：US09807670B2

公开(公告)日：2017-10-31

申请号：US13828378

申请日：2013-03-14

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

Inventor： Severine Vermande ,  Fabrice Vermande ,  Etienne Maynier

IPC: H04W40/20 ,  H04B7/185

CPC classification number: H04W40/20 ,  H04B7/18506

Abstract: In a communications network including aircraft in flight and at least one ground station, which constitute communication nodes of the network, data are transmitted from a source node to a destination node following a non-predetermined path through the network that includes at least one node which is a so-called intermediate aircraft. Before transmitting data from a transmitting node to at least one receiving node, it envisages a step of selecting the receiving node defining a portion of the path without knowledge of the next portion of the path.

公开(公告)号：US20170171112A1

公开(公告)日：2017-06-15

申请号：US15376606

申请日：2016-12-12

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

Inventor： Jean-François SAINT-ETIENNE ,  Juan Lopez

IPC: H04L12/931 ,  H04L12/935 ,  H04L12/933 ,  H04L29/08 ,  H04L12/46

CPC classification number: H04L49/351 ,  H04L12/40006 ,  H04L12/4625 ,  H04L12/4641 ,  H04L49/15 ,  H04L49/30 ,  H04L67/12 ,  H04L2012/4028

Abstract: A subscriber of a deterministic Ethernet communication network using virtual links including a first receiver, a first transmitter, a first memory to record a configuration table relating to a set of virtual links that the subscriber can receive and/or retransmit. A processing unit is configured to implement at least one application, a reception function to receive data frames received by the first receiver, to accept the reception only of the frames corresponding to virtual links belonging to the set of virtual links and to transmit these frames to a sorting function to transmit the data frames received to the application and/or to a transmission function to dispatch the data frames received to the first transmitter while complying with Bandwidth Allocation Gap (BAG) constraints associated with the corresponding virtual links.

公开(公告)号：US09672498B2

公开(公告)日：2017-06-06

申请号：US14715269

申请日：2015-05-18

Applicant: Airbus (S.A.S.)

Inventor： Dang Nguyen Manh ,  David Marty ,  Gerald Bidault ,  Massimiliano Di Santo ,  Fabien Fleurey

IPC: B64F5/00 ,  G06Q10/00

CPC classification number: G06Q10/20

Abstract: Methods, systems, and computer readable media for managing periodic aircraft maintenance planning are provided. In some aspects, a method occurs at a maintenance platform server including a processor. The method includes providing one or more maintenance related object (MO), wherein each of the one or more MO represents one or more maintenance related task that includes criteria graphically depicted at an interface. In another aspect, the method further includes manipulating the criteria of the one or more maintenance related task represented by the one or more MO at the interface.

公开(公告)号：US20170011638A1

公开(公告)日：2017-01-12

申请号：US15206332

申请日：2016-07-11

Applicant: AIRBUS GROUP INDIA PRIVATE LIMITED ,  AIRBUS (S.A.S.) ,  AIRBUS OPERATIONS (S.A.S.)

Inventor： ASHUTOSH AGRAWAL ,  Georges Myczkowski ,  Brendan Clarke ,  Nicolas Landrin ,  Lucas Babelaere ,  Nathalie Willig ,  Diego Alonso-Tabares

IPC: G08G5/00 ,  G08G5/02

CPC classification number: G08G5/0095 ,  G06Q10/063 ,  G06Q10/0631 ,  G06Q10/06312 ,  G06Q10/06315 ,  G06Q10/06316

Abstract: A system for monitoring scheduled turnaround activities and alerting on time deviation from the scheduled turnaround activities is disclosed. The system includes a ground computing station system, an aircraft on-board system, a cloud, and user interface. The cloud is communicatively coupled to the ground station computing system and the aircraft on-board system. The cloud includes processor and memory. The memory includes an analytics module to obtain actual start and end time stamps associated with scheduled turnaround activities, from touchdown to takeoff of an aircraft, from aircraft on-board systems and a ground station system. The analytics module to determine time deviation of scheduled turnaround activities by analyzing the obtained actual start and end time stamps. The user interface to present each scheduled turnaround activity and determined time deviation of the scheduled turnaround activities.

Abstract translation: 公开了一种用于监视预定的周转活动并提醒与预定的周转活动的时间偏差的系统。 该系统包括地面计算站系统，飞机机载系统，云端和用户接口。 云通信耦合到地面站计算系统和飞机机载系统。 云包括处理器和内存。 内存包括一个分析模块，用于获得与预定的周转活动相关的实际开始和结束时间戳，从触地飞机起飞，飞机机载系统和地面站系统。 分析模块通过分析获得的实际开始和结束时间戳来确定预定周转活动的时间偏差。 用户界面提供每个预定的周转活动并确定预定周转活动的时间偏差。

公开(公告)号：US20160176496A1

公开(公告)日：2016-06-23

申请号：US14977121

申请日：2015-12-21

Applicant: AIRBUS (S.A.S.) ,  Airbus Operations S.L.

Inventor： Zengli Han ,  Haifeng Chen ,  Ming Luo ,  Angel Postigo-Rodriguez ,  Daniel De-La-Sen-Perez ,  Laure Partouche

IPC: B64C1/14 ,  E05C3/12 ,  E06B3/04

CPC classification number: B64C1/1446 ,  B64C3/34 ,  E05C3/124 ,  E06B3/04

Abstract: The present invention relates to a door for closing an opening in a structure, including: a body arranged to be capable of abutting against a first side of the opening; at least one clamping member configured to be capable of abutting against an opposite second side of the opening; and a fastener arranged to fasten or release the clamping member relative to the body. The clamping member is moveable relative to the body between a first position where the clamping member abuts against the second side of the opening so as to clamp the structure between the body and the clamping member and a second position where the clamping member allows the door to be opened. The present invention further relates to an aircraft including the above door.

Abstract translation: 本发明涉及一种用于关闭结构中的开口的门，包括：主体，其能够抵靠开口的第一侧; 至少一个夹紧构件构造成能够抵靠所述开口的相对的第二侧; 以及紧固件，其布置成相对于主体紧固或释放夹紧构件。 夹紧构件可相对于主体在第一位置和第二位置之间移动，该第一位置与夹紧构件抵靠开口的第二侧之间，以便将构件夹在主体和夹紧构件之间，并且夹紧构件允许门 被打开 本发明还涉及一种包括上述门的飞行器。

公开(公告)号：US20160075445A1

公开(公告)日：2016-03-17

申请号：US14841237

申请日：2015-08-31

Applicant: Airbus (S.A.S.)

Inventor： Christophe CROS ,  Alain FONTAINE

IPC: B64D45/00 ,  B64D47/06 ,  B64D17/00 ,  G01S5/02

CPC classification number: B64D45/00 ,  B64D17/00 ,  B64D25/20 ,  B64D47/06 ,  B64D2045/0065 ,  G01S5/0231 ,  Y02T50/53

Abstract: An aircraft including a fuselage having an outer face on which is fixed a second interface, at least one emergency beacon including a base having a first interface to cooperate with the second interface for fixing of the base onto the outer face, and a casing housing a control unit, a radio transmitter for transmitting a distress radio signal and detector to detect abnormal aircraft behavior, and fixing structure to take up a fixation position to ensure fixing of the casing onto the base or a separation position, in which it does not ensure fixing of the casing onto the base, the transition from the fixation position to the separation position being ordered by the control unit when the detector detect an abnormal behavior.

Abstract translation: 一种飞机，包括具有外表面的机身，固定有第二接口，至少一个紧急信标，包括具有第一接口的基座，所述第一接口与所述第二接口协作以将所述基座固定到所述外表面上;以及壳体， 控制单元，用于发送遇险无线电信号的无线电发射机和用于检测异常飞行器行为的检测器，以及固定结构以占据固定位置，以确保将壳体固定到基座或分离位置，其中它不能确保固定 当检测器检测到异常行为时，由控制单元对从固定位置到分离位置的过渡进行排序。

公开(公告)号：US20160031570A1

公开(公告)日：2016-02-04

申请号：US14808863

申请日：2015-07-24

Applicant: Airbus (S.A.S.)

Inventor： Bernard ORDY ,  Alexis JACQUEMIN ,  Sylvain CHAMAILLARD ,  Eric JASTRZEBSKI

IPC: B64F5/00 ,  G06F17/28 ,  G06Q10/06 ,  G06F17/27 ,  G10L15/26

CPC classification number: G06F17/28 ,  B64F5/40 ,  G02B27/0093 ,  G02B2027/014 ,  G02B2027/0178 ,  G05B19/418 ,  G05B2219/35453 ,  G05B2219/35495 ,  G06F3/016 ,  G06F11/32 ,  G06F17/2785 ,  G06Q10/06398 ,  G06Q10/20 ,  G10L15/1822 ,  G10L15/26

Abstract: The disclosure herein relates to ensuring the mutual understanding between a remote maintenance support engineer guiding a maintenance engineer intervening on an aircraft, and concerns a system of prevention comprising first and second communication terminals to enable the maintenance engineer and remote maintenance support engineer to exchange information with each other, the information including oral guidance instructions given by the maintenance support engineer and oral responses given by the maintenance engineer relating to the execution of the instructions, a voice recognition device configured for transforming the oral instructions and responses into textual instructions and responses, a semantic analysis device configured for comparing the textual instructions with the textual responses in order to detect any possible inconsistency between the instructions and the responses, and a warning device configured for generating a warning when an inconsistency is detected between the instructions and the responses.

Abstract translation: 本文的公开内容涉及确保引导在飞行器上进行维护的维护工程师的远程维护支持工程师之间的相互理解，并涉及包括第一和第二通信终端的预防系统，以使得维护工程师和远程维护支持工程师能够与 彼此，所述信息包括由维护支持工程师给出的口头指导指令和由维护工程师提供的关于执行指令的口头答复;语音识别设备，其被配置为将口头指令和响应转换为文本指令和响应， 语义分析装置，其被配置为将文本指令与文本响应进行比较，以便检测指令和响应之间的任何可能的不一致;以及警告装置，被配置为当在所述指令与所述响应之间检测到不一致时产生警告 说明和回应。

公开(公告)号：US20150329193A1

公开(公告)日：2015-11-19

申请号：US14529404

申请日：2014-10-31

Applicant: AIRBUS S.A.S.

Inventor： Wei SUN ,  Hong CHEN

IPC: B64C1/06

CPC classification number: B64C1/069 ,  B64C9/02 ,  F16C11/02 ,  F16C2326/43

Abstract: The present invention relates to a bending-sustaining joint and an aircraft including the same. The bending-sustaining joint includes a body for attaching to a support structure, the body having a first end with a first bore including an internal thread portion and a non-threaded portion; a sleeve including a fitting portion which can be fit into the non-threaded portion of the first bore, a bearing portion for bearing a born member and a through hole; and a bolt member including a thread section and a bolt head which can abut an end face of the sleeve, the thread section of the bolt member being capable of passing through the through hole of the sleeve and being screwed into the internal thread portion of the first bore so as to secure the sleeve to the body.

Abstract translation: 本发明涉及一种弯曲维持接头和包括该弯曲维持接头的飞行器。 所述弯曲维持接头包括用于附接到支撑结构的本体，所述本体具有第一端，所述第一端具有包括内螺纹部分和非螺纹部分的第一孔; 套筒，其包括可以装配到第一孔的非螺纹部分中的装配部分，用于承载出生构件的轴承部分和通孔; 以及螺栓构件，其包括螺纹部和螺栓头，所述螺栓部能够抵接所述套筒的端面，所述螺栓构件的螺纹部能够穿过所述套筒的通孔并被螺纹连接到所述套筒的内螺纹部分中 第一孔，以便将套筒固定到身体上。

公开(公告)号：US20150259067A1

公开(公告)日：2015-09-17

申请号：US14660268

申请日：2015-03-17

Applicant: Airbus S.A.S. ,  Airbus Operations GmbH

Inventor： Bruno Saint-Jalmes ,  André Rezag ,  Jason Zaneboni ,  Markus Schumacher ,  Andrew Muin ,  Cord Haack ,  Michael Carr

IPC: B64D11/00 ,  B64D11/06 ,  B64C1/18

CPC classification number: B64D11/003 ,  B64C1/18 ,  B64D11/00 ,  B64D11/0015 ,  B64D11/00154 ,  B64D11/06 ,  B64D11/0601 ,  B64D11/0604 ,  B64D11/0611 ,  B64D11/0626 ,  B64D11/0627 ,  B64D11/0631 ,  B64D11/0639 ,  B64D11/06395 ,  B64D11/0649 ,  B64D11/0696 ,  B64D2011/0046 ,  B64D2011/0053 ,  Y02T50/46 ,  Y10T29/49826

Abstract: A module for an aircraft has a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane.

Abstract translation: 用于飞行器的模块具有机身结构和限定地面平面的地板元件。 模块包括适于安装功能元件的框架装置，并且框架装置适于在地板平面中的第一位置处附接到飞机的地板元件。