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公开(公告)号：US20140175224A1
公开(公告)日：2014-06-26
申请号：US14138551
申请日：2013-12-23
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
Abstract: An aircraft nose comprising a primary fuselage structure, and housed inside said structure, a cockpit, and an avionics bay containing a plurality of avionics racks designed to receive electrical and/or electronic equipment. The cockpit and the avionics bay are each made in the form of a distinct module that is suitable for being installed in a single operation inside the primary fuselage structure. The use of modules for integrating in the aircraft nose makes it possible to reduce considerably the time required for fitting out the nose on the final assembly line of the aircraft.
Abstract translation: 包括主机架结构并且容纳在所述结构内的飞行器鼻架，驾驶舱和航空电子设备舱，其包含设计成接收电和/或电子设备的多个航空电子设备架。 驾驶舱和航空电子设备舱均采用独特模块的形式，适合安装在主机身结构内的单一操作中。 使用用于集成在飞机鼻部中的模块可以大大减少在飞机的最终装配线上安装鼻子所需的时间。
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公开(公告)号：US20140175220A1
公开(公告)日：2014-06-26
申请号：US14106113
申请日：2013-12-13
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
CPC classification number: B64D43/00 , B64C1/1476 , B64C1/32
Abstract: The present invention relates to an aircraft cockpit with a double flight deck in which a central pane of a windscreen can be removed in order to at least partially clear an opening in order to constitute an emergency exit and ensure natural ventilation of the cockpit. Moreover, a central portion of a glare shield and of a flight station instrument panel are optionally moveable in order to facilitate access to the opening in the event of the need for emergency evacuation.
Abstract translation: 本发明涉及具有双飞行甲板的飞行器驾驶舱，其中可以移除挡风玻璃的中央窗格以便至少部分地清除开口以构成紧急出口并确保驾驶舱的自然通风。 此外，眩光屏蔽和飞行台仪表板的中心部分可选地可移动，以便在需要紧急撤离的情况下方便进入开口。
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公开(公告)号：US09505483B2
公开(公告)日：2016-11-29
申请号：US14348093
申请日：2012-09-27
Applicant: Airbus Operations (SAS)
Inventor： Bernard Guering , Yves Durand
CPC classification number: B64C1/14 , B64C1/061 , B64C1/10 , B64C1/36 , B64C25/04 , B64C25/10 , B64C25/14
Abstract: A forward part of an aircraft comprising a fuselage and a landing gear well housing a forward landing gear comprising a breaker strut designed to adopt an extended configuration when the landing gear is extended, configuration in which said breaker strut lies in a strut plane parallel to the transverse direction of the forward part. The forward part comprises a transverse beam resisting strut reactions located above the landing gear well and mounted on the fuselage at its two ends, the beam having a globally rectangular cross-section, in which the median plane parallel to the length of the rectangle is coincident with said strut plane.
Abstract translation: 一种飞机的前部，其包括机身和起落架井，该起落架井容纳前起落架，该前起落架包括设计成当起落架延伸时采用延伸构型的断路器支柱，其中所述断路器支柱位于平行于 前部横向。 前部包括位于起落架井上方的横向梁抵抗支柱反应，并在其两端安装在机身上，该梁具有全局矩形横截面，其中平行于矩形长度的中间平面重合 与支柱平面。
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4.发明申请Front aircraft sealed bottom comprising recesses for housing cockpit equipment 有权前部飞机密封底部包括用于容纳驾驶舱设备的凹部公开(公告)号：US20140203143A1
公开(公告)日：2014-07-24
申请号：US14108718
申请日：2013-12-17
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guerring
Abstract: A leaktight nose cone backplate for an aircraft having a first side oriented towards a radome zone intended to house a mobile antenna, and a second side opposite the first side and oriented towards a cockpit of the aircraft. The second side has at least one recess intended to receive at least one piece of cockpit equipment, each recess being partly delimited by a backplate structure forming a protrusion on the first side.
Abstract translation: 一种用于飞行器的密封鼻锥背板，其具有朝向朝向要容纳移动天线的天线罩区域的第一侧，以及与第一侧相对的第二侧并朝向飞行器的驾驶舱。 第二侧面具有用于容纳至少一个驾驶舱设备的至少一个凹部，每个凹部部分地由在第一侧上形成突起的背板结构限定。
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5.发明申请PIECE OF FURNITURE FOR AN AIRCRAFT INCLUDING MEANS FOR DISTRIBUTING A CARRIAGE BETWEEN TWO SECTIONS 有权用于飞机的家具包括用于分配两部分之间的运输的手段公开(公告)号：US20140166806A1
公开(公告)日：2014-06-19
申请号：US14106216
申请日：2013-12-13
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
IPC: B64D11/04
CPC classification number: B64D11/04 , B64D11/0007
Abstract: A piece of furniture for an aircraft, including a plurality of carriages a first section forming an interface of use for a user with which at least one carriage may be taken and/or deposited in the piece of furniture and a second section allowing the said carriages to be circulated along at least first and second main directions substantially perpendicular to each other, at least in a plane of the aircraft for storing and/or delivering to the user at least one carriage, the first section and/or the second section including an arrangement for distributing at least one carriage from the second section towards the first section and vice versa.
Abstract translation: 一种用于飞行器的家具，包括多个滑架，第一部分形成用于使用者的接口，至少一个托架可以与该家具相连和/或放置在该家具中;以及第二部分，允许所述托架 至少在飞行器的平面中沿着至少基本上彼此垂直的至少第一和第二主方向循环，以便向用户存储和/或传送至少一个滑架，第一部分和/或第二部分包括 用于从第二部分向第一部分分配至少一个托架的布置，反之亦然。
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Patent Agency Ranking
6.发明申请公开(公告)号：US20140165285A1
公开(公告)日：2014-06-19
申请号：US14132982
申请日：2013-12-18
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
IPC: B64D11/02
Abstract: A toilet area for an aircraft cabin comprising an access door and housing a toilet bowl. The toilet area also comprises an evacuation exit, the access door occupying a closed position in the toilet area in a toilet configuration and a folded position in the toilet area in an evacuation configuration. Usage in particular in a flying wing aircraft is provided.
Abstract translation: 一种用于飞机机舱的卫生间区域，其包括通道门和容纳马桶。 厕所区域还包括撤离出口，进入门在马桶构造中占据马桶区域中的关闭位置，并且在抽空构造中在厕所区域中的折叠位置。 特别提供飞翼飞机的使用。
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7.发明申请Method for installing a wiring harness in an aircraft and tool for implementing said method 审中-公开用于在飞行器和工具中安装线束的方法，用于实现所述方法公开(公告)号：US20140145128A1
公开(公告)日：2014-05-29
申请号：US14087064
申请日：2013-11-22
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
IPC: H02G1/06
Abstract: A method for installing a wiring harness in an aircraft. The method comprises using cables having first ends secured to the harness and winding means onto each of which is wound one of said cables so as to lift up said harness by exerting a tensile force. The first ends of the cables are distributed along at least a section of the harness so as to distribute the tensile forces over the section.
Abstract translation: 一种在飞行器中安装线束的方法。 该方法包括使用具有固定到线束的第一端和缠绕装置的电缆，其中每个绕线装置缠绕所述电缆之一，以便通过施加张力来提升所述线束。 电缆的第一端沿着线束的至少一部分分布，以便在该部分上分布张力。
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8.发明授权公开(公告)号：US10186848B2
公开(公告)日：2019-01-22
申请号：US14087064
申请日：2013-11-22
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
Abstract: A method for installing a wiring harness in an aircraft. The method comprises using cables having first ends secured to the harness and winding means onto each of which is wound one of said cables so as to lift up said harness by exerting a tensile force. The first ends of the cables are distributed along at least a section of the harness so as to distribute the tensile forces over the section.
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公开(公告)号：US09359084B2
公开(公告)日：2016-06-07
申请号：US14138588
申请日：2013-12-23
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
CPC classification number: B64D43/00 , B64C1/18 , B64C2001/009 , B64F5/10 , Y10T29/49826
Abstract: An integral avionics bay module. The module has a structure that has an integral cabin floor on top that closes the structure. Installing such an integral avionics bay structure in a single operation inside a primary fuselage structure considerably reduces the integration time on the final assembly line for the aircraft.
Abstract translation: 一个完整的航空电子海湾模块。 该模块具有在顶部具有整体的舱室结构的结构，其关闭结构。 在主机身结构内的单一操作中安装这样一个整体的航空电子设备舱结构大大减少了飞机最终装配线上的集成时间。
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10.发明授权Ventilation system, air blowing and extraction circuits of such a system, as well as an aircraft avionics bay 有权通风系统，这种系统的吹风和抽风回路，以及飞机航空电子海湾公开(公告)号：US09216809B2
公开(公告)日：2015-12-22
申请号：US13628153
申请日：2012-09-27
Applicant: Airbus Operations SAS
Inventor： Bernard Guering , Yves Durand
CPC classification number: B64C1/18 , B64D13/00 , B64D2013/0614 , H05K7/20554
Abstract: A ventilation system for an avionics bay has two strut assemblies for stiffening the floor of the cockpit, each strut assembly being arranged symmetrically regarding to the central plane of the aircraft, and means of distribution of the blowing air in the cabinets of the bay from the strut assemblies. The extraction circuit includes exhaust ducts integrated in the cabinets and couples together by tight inter-cabinets junctions in an overall configuration of maximized compactness.
Abstract translation: 用于航空电子设备舱的通风系统具有两个用于加强驾驶舱地板的支柱组件，每个支柱组件关于飞行器的中心平面对称地布置，以及将吹风空气分配在舱的机柜中的装置， 支柱组件。 提取电路包括集成在机柜中的排气管道，并通过紧密的机柜间连接在一起，以最大的紧凑性的整体结构。
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