公开(公告)号：EP3233635A1

公开(公告)日：2017-10-25

申请号：EP15820028.7

申请日：2015-12-10

申请人： FACC AG

发明人： KAMMERER, Bernhard ,  KOLETNIK, Sandi ,  SCHÖRKHUBER, Jakob ,  KRALOVEC, Christoph

IPC分类号： B64D11/00 ,  B64D13/00

CPC分类号： B64D11/003 ,  B64D11/00 ,  B64D2011/0053 ,  B64D2013/003 ,  B64D2231/025 ,  Y02T50/46

摘要： The invention relates to an overhead luggage compartment (1) for aircraft (F), comprising: a trough (3) for accommodating pieces of luggage (L), which trough can be pivoted about an axis of rotation (A) between a closed position and an open position; an enclosure (4), which encloses the trough (3) in the closed position and which has devices (5) arranged thereon for fastening to a supporting structure (S) of the aircraft (F) and has a suspension device (6) for a passenger service unit (7); and a closure element (8) for holding the trough (3) in the closed position. In order to create an easily mountable overhead luggage compartment (1) having the lowest possible weight and the greatest possible volume for accommodating the pieces of luggage (L), the enclosure (4) is formed by two frame parts (9) arranged lateral to the trough (3), which frame parts (9) are connected to each other by means of cross-braces (10), and the fastening apparatuses (5) and the suspension device (6) for the passenger service unit (7) and at least one stop element (25) for limiting the open position of the trough (3) are arranged on the frame parts (9).

摘要翻译： 本发明涉及一种用于飞机（F）的高架行李箱（1），包括：用于容纳行李件（L）的槽（3），所述槽能够围绕旋转轴线（A）在关闭位置 和一个开放的位置; （4），其在关闭位置封闭槽（3），并具有布置在其上的用于紧固到飞机（F）的支撑结构（S）的装置（5），并且具有悬挂装置（6） 一个乘客服务单元（7）; 和用于将槽（3）保持在关闭位置的封闭元件（8）。 为了形成具有尽可能小的重量和最大可能容积以容纳行李箱（L）的可轻松安装的顶部行李箱（1），外壳（4）由两个框架部件（9）形成，所述两个框架部件 （9）通过交叉撑杆（10）彼此连接的槽（3）以及用于乘客服务单元（7）的紧固装置（5）和悬挂装置（6）以及 在框架部件（9）上布置有用于限制槽（3）的打开位置的至少一个止挡元件（25）。

公开(公告)号：EP3168152A1

公开(公告)日：2017-05-17

申请号：EP15194541.7

申请日：2015-11-13

申请人： Goodrich Lighting Systems GmbH

发明人： HESSLING-von HEIMENDAHL, Andre ,  BECKER, Stefan

IPC分类号： B64D11/00

CPC分类号： B64D11/00 ,  B64D13/00 ,  B64D47/00 ,  B64D47/02 ,  B64D2011/0053 ,  B64D2013/003 ,  B64D2045/007 ,  B64D2231/025 ,  Y02T50/46

摘要： An overhead aircraft passenger service unit (2), which is configured to be placed above the passenger seats within an aircraft cabin, comprises at least one cavity (9) for housing at least one oxygen mask (16) and at least one removable cover (10), which at least partially covers an opening of the cavity (9). The removable cover (10) houses and/or supports at least one functional component (4, 6, 8, 12, 14).

摘要翻译： 被配置为放置在飞机机舱内乘客座位上方的高架飞机乘客服务单元（2）包括用于容纳至少一个氧气面罩（16）的至少一个空腔（9）以及至少一个可移除盖（ 10），其至少部分地覆盖空腔（9）的开口。 可移除盖（10）容纳和/或支撑至少一个功能部件（4,6,8,12,14）。

公开(公告)号：EP3141286A1

公开(公告)日：2017-03-15

申请号：EP16185497.1

申请日：2016-08-24

申请人： The Boeing Company

发明人： FILES, Joe ,  LOGUE, Adam Arthur ,  CHI, Meiling ,  RHYNARD, Steven Ellis ,  SMITHSON, Lance

IPC分类号： A62B25/00

CPC分类号： B64D11/00 ,  A62B18/02 ,  A62B25/005 ,  B64D2231/025

摘要： An oxygen box (22) is secured in an oxygen box hole through a panel of an aircraft cabin by fasteners (24) that are positioned in an interior volume of the oxygen box and are inserted through holes (48) in a back wall of the oxygen box that are aligned with fastener openings (74) in an exterior bracket (18) positioned behind the panel and behind the oxygen box opening where the fasteners (24) are received by the fastener openings in the exterior bracket and the fasteners removably attach the oxygen box to the exterior bracket.

摘要翻译： 氧箱（22）通过由紧固件飞机机舱的面板获得固定在氧气箱（24）并定位在氧气箱的内部体积，并通过在所述后壁的孔（48）被插入 氧箱做了与紧固件开口（74）到位于面板后面和氧气箱开口在紧固件（24）由所述紧固件开口在外部托架接收和紧固件可拆卸地附接的后面外部托架（18）对齐 氧箱到外部托架。

公开(公告)号：EP3138607A1

公开(公告)日：2017-03-08

申请号：EP16185404.7

申请日：2016-08-23

申请人： Airbus Group India Private Limited

发明人： SHARMA, ANURAG

IPC分类号： A62B7/14 ,  A62B18/08 ,  G02B27/01

CPC分类号： G06T19/006 ,  A62B18/02 ,  B64D2231/025 ,  G02B27/0093 ,  G02B27/017 ,  G06F3/013

摘要： An aviation mask is disclosed which includes an augmented reality visor, sensors, and a display computational unit. The sensors are communicatively connected to the augmented reality visor. The sensors detect a portion of a cockpit area of an aircraft that is viewed by an aircraft crew member wearing the augmented reality visor during a vision obscured emergency. The display computational unit is communicatively connected to the augmented reality visor and the sensors. The display computational unit projects a prestored image associated with the portion of the cockpit area in front of the augmented reality visor. Further, the display computational unit superimposes the prestored image over the portion of the cockpit area viewed by the aircraft crew member. The superimposed prestored image being viewed by the aircraft crew member through the augmented reality visor to identify objects in the portion of the cockpit area during the vision obscured emergency.

摘要翻译： 公开了一种包括增强现实面罩，传感器和显示计算单元的航空面罩。 传感器通信连接到增强现实面罩。 这些传感器检测飞机的驾驶舱区域的一部分，该飞机的驾驶舱区域在视觉模糊的紧急情况下由穿着增强现实遮阳板的飞机机组人员观看。 显示计算单元通信地连接到增强现实面罩和传感器。 显示计算单元投影与增强现实面罩前面的驾驶舱区域的部分相关联的预存图像。 此外，显示计算单元将预先存储的图像叠加在驾驶舱区域由飞机机组成员观看的部分上。 飞机机组人员通过增强现实遮阳板查看叠加的预先存储的图像，以在视觉期间识别驾驶舱区域中的物体遮蔽了紧急情况。

公开(公告)号：EP3111996A1

公开(公告)日：2017-01-04

申请号：EP15174644.3

申请日：2015-06-30

申请人： Airbus Operations GmbH

发明人： Bricard, Patrick ,  Martin, Timo

IPC分类号： A62B7/14 ,  B64D13/00

CPC分类号： A62B7/14 ,  A62B7/02 ,  A62B9/006 ,  A62B9/04 ,  A62B18/02 ,  B64D13/00 ,  B64D2231/00 ,  B64D2231/025

摘要： The present invention relates to an oxygen supply system (1) for providing an adequate oxygen supply mode in an aircraft, having a preventive oxygen supply system (2) comprising an oxygen source (20);a preventive oxygen dispensing unit (21) being connectable to said oxygen source (20); a cabin altitude detection device (23); and a preventive oxygen control device (22) being adapted to provide at least the following modes: a pre-wear mode for providing no oxygen of said oxygen source (20) to said preventive oxygen dispensing unit (21) but normal cabin air; a pre-oxygenation mode for providing a predetermined rate of oxygen of said oxygen source (20) to said preventive oxygen dispensing unit (21) being sufficient for generating a pre-oxygenation condition of the user; and a decompression mode for providing high concentrated oxygen of said oxygen source (20) to said preventive oxygen dispensing unit (21) being sufficient for ensuring a minimum oxygenation of the user; wherein said preventive oxygen control device (22) automatically switches to the decompression mode in case a predetermined cabin altitude threshold is detected by said cabin altitude detection device (23). Further, the present invention relates to a respective method for providing an adequate oxygen supply mode using such an oxygen supply system (1).

摘要翻译： 本发明涉及一种在氧气供应系统（1），用于在飞机在充足的氧气供应模式中提供，具有预防供氧系统（2）在氧源，其包含（20）;预防氧气分配单元（21）可连接 所述氧源（20）; 一个座舱高度检测装置（23）; 和预防性氧控制装置（22）是angepasst以提供至少下列模式：磨损预方式用于提供没有所述氧气源（20）向所述预防性氧气分配单元（21），但正常座舱空气的氧; 一个氧合前模式用于提供所述氧气源（20）向所述预防性氧气分配单元（21）是足够的，用于产生所述用户的氧合先决条件的氧的预定速率; 和减压模式到所述预防性氧气分配单元（21）是足以确保用户的最小氧合提供所述氧气源（20）的高浓度氧; worin说预防性氧控制装置（22）自动地切换到在壳体的预定舱室纬度阈由所述机舱高度检测装置（23）检测到的解压缩模式。 此外，本发明涉及一种方法，用于提供使用搜索到的氧气供应系统（1）足够的氧供应模式respectivement。

公开(公告)号：EP2873882A4

公开(公告)日：2015-08-19

申请号：EP13816948

申请日：2013-07-04

申请人： THK CO LTD

发明人： MOCHIZUKI HIROAKI ,  HOSAKA EIJI ,  KURIBAYASHI HIROOMI ,  KANEKO AKITO

IPC分类号： F16C29/06 ,  B64D11/00 ,  F16C29/00 ,  F16C29/12 ,  F16M13/02

CPC分类号： F16M13/022 ,  B64D11/00 ,  B64D2231/025 ,  F16C29/004 ,  F16C29/008 ,  F16C29/0623 ,  F16C29/063 ,  F16C2326/43 ,  F16M13/027

摘要： Provided is a moving unit (1) that enables a movable body (41) to be smoothly moved along guide tracks (2) for guiding the movable body (41) across joints between a plurality of track rails (21) arranged in series so as to serve as the guide tracks. The moving unit (1) includes: the pair of guide tracks (2) laid in parallel to each other; a plurality of moving blocks (3) being two or more moving blocks (3) assembled to each of the guide tracks and being freely movable along the guide tracks; and the movable body (41) fixed to the moving blocks. The track rails (21) arranged in series serve as the guide tracks, and each have a guide surface (25) formed along a longitudinal direction of each of the track rails. The moving blocks (3) each include contact elements (31) configured to travel on the guide surface while passing across joint clearances (L) each being formed between the track rails arranged in series. When one of the moving blocks (3) is positioned at any one of the plurality of joint clearances (L) formed on the pair of guide tracks (2), another of the moving blocks is not positioned at another of the joint clearances.

公开(公告)号：EP2665525A4

公开(公告)日：2014-07-16

申请号：EP12736174

申请日：2012-01-11

申请人： AVOX SYSTEMS INC

发明人： GILL CHRISTOPHER F

IPC分类号： A62B25/00 ,  B64D11/00

CPC分类号： A62B25/005 ,  B64D2231/025

公开(公告)号：EP2665525A2

公开(公告)日：2013-11-27

申请号：EP12736174.9

申请日：2012-01-11

申请人： AVOX Systems Inc.

发明人： GILL, Christopher, F.

IPC分类号： A62B18/02 ,  A62B7/10 ,  A62B9/00

CPC分类号： A62B25/005 ,  B64D2231/025

摘要： The present invention provides a method and apparatus for storing breathing masks in a tall and narrow space and deploying the masks from that space. The apparatus may be embodied as a removable cartridge containing a breathing mask assembly housed within a frame. The cartridge is comprised of a first side and second side which can move relative to the frame. The first side includes a hinge. In operation, the cartridge slides relative to the frame and rotatably opens via the hinge after the cartridge substantially exits the frame. A breathing mask is released to a user after the first and second halves rotatably separate.

公开(公告)号：EP2525874A1

公开(公告)日：2012-11-28

申请号：EP10714677.1

申请日：2010-01-22

申请人： Intertechnique

发明人： BRUCKERT, Sébastien

IPC分类号： A62B7/14 ,  B64D10/00

CPC分类号： A62B18/084 ,  A62B9/02 ,  A62B18/10 ,  A62B25/00 ,  B64D10/00 ,  B64D2231/025

摘要： A breathing assembly (1) for aircraft comprising:—a breathing mask (2) to be connected to a source of breathing gas,—a stowage box (10) forming a receptacle for receiving the breathing mask (2) in a stowage position, and—a valve assembly (20) comprising a valve (32) having an open position in which the valve (32) allows the feed of breathing gas to the breathing mask (2) and a closed position in which the valve (32) prevents the feed of breathing gas to the breathing mask (2), the valve assembly (20) being supported by the breathing mask (2), and—a retaining element (14) connected to the stowage box (10) and cooperating with the valve assembly (20) to maintain the valve (32) in the closed position when the breathing mask (2) is in the stowage position.

公开(公告)号：EP2229319B1

公开(公告)日：2011-05-18

申请号：EP08719869.3

申请日：2008-01-04

申请人： INTERTECHNIQUE

发明人： BACHELARD, Léopoldine ,  BRÜCKERT, Sébastien

IPC分类号： B64D11/00

CPC分类号： B64D11/00 ,  A62B7/14 ,  A62B25/005 ,  B64D2231/025

摘要： A device for oxygen supply of a user in an aircraft comprising a breathing mask (20), a stowage box (1 ) for the breathing mask and an oxygen supply hose (22) having one end connected to the stowage box and the other end connected to the breathing mask, wherein the device further comprises means (3) to fix the stowage box in a ceiling of the aircraft, an aperture on the bottom side of the stowage box closed by a door (7) and a leash (28) connected to the stowage box by one end and to the breathing mask by the other end so that, when the door is open, the mask falls and is kept hovered by the oxygen supply hose and the leash.