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1. 发明授权

US09045235B2 Service device, passenger service unit, fuselage of an aircraft, method for installing the service device 有权
标题翻译：服务设备，乘客服务单元，飞机机身，安装服务设备的方法
公开(公告)号：US09045235B2
公开(公告)日：2015-06-02
申请号：US13955214
申请日：2013-07-31
申请人： INTERTECHNIQUE
发明人： Wolfgang Rittner , Hasso Weinmann , Günter Boomgaarden , Andreas Westphal , Rüdiger Meckes , Werner Granzeier , Torsten Kanitz , Hasko Rose , Alexander Berschin
IPC分类号： B64D47/02 , F21V33/00 , B60Q3/02
CPC分类号： B64D47/02 , B60Q3/44 , B60Q2500/20 , B64D11/00 , B64D13/00 , B64D2011/0053 , B64D2013/003 , F21V33/0092 , Y10T29/49117
摘要： The invention relates to a service device having a system of a gasper module and a lighting module for a passenger service unit of an aircraft, comprising: a lighting source in a housing of the lighting module for providing light and a gasper orifice in a housing of the gasper module for supply of gasper air, wherein the lighting module and the gasper module are assembled in a housing assembly of the service device, wherein the housing assembly is adapted to hold the lighting module and the gasper module essentially around an axis (Z) of the housing assembly. According to the invention the lighting module and the gasper module are separated from each other by a housing assembly bearing part, and a force transmission is applicable to the lighting module and the gasper module for independent movement of at least one of the lighting module and the gasper module relative to the bearing part, and wherein the gasper module housing and the lighting module housing are separately form fitted to the bearing part by a positive locking.
摘要翻译：本发明涉及一种具有气垫模块系统和飞机乘客服务单元的照明模块的服务设备，包括：照明模块的壳体中的照明源，用于在照明模块的壳体内提供光线，用于提供气流空气的气体模块，其中所述照明模块和所述吸气模块组装在所述维修设备的壳体组件中，其中所述壳体组件适于将所述照明模块和所述气体模块基本上围绕轴线（Z）的房屋组件。根据本发明，照明模块和吸气模块通过壳体组件支承部件彼此分开，并且力传递可应用于照明模块和气体模块，用于独立移动照明模块和照明模块中的至少一个气体模块相对于轴承部分，并且其中气体模块壳体和照明模块壳体通过正向锁定分开地装配到轴承部件。

2. 发明申请

US20150036368A1 Service device, Passenger Service Unit, Fuselage of an Aircraft, Method for Installing the Service Device 有权
标题翻译：服务设备，乘客服务单位，飞机机身，安装服务设备的方法
公开(公告)号：US20150036368A1
公开(公告)日：2015-02-05
申请号：US13955214
申请日：2013-07-31
申请人： INTERTECHNIQUE
发明人： Wolfgang Rittner , Hasso Weinmann , Günter Boomgaarden , Andreas Westphal , Rüdiger Meckes , Werner Granzeier , Torsten Kanitz , Hasko Rose , Alexander Berschin
IPC分类号： B64D47/02
CPC分类号： B64D47/02 , B60Q3/44 , B60Q2500/20 , B64D11/00 , B64D13/00 , B64D2011/0053 , B64D2013/003 , F21V33/0092 , Y10T29/49117
摘要： The invention relates to a service device (1000) having a system of a gasper module (100) and a lighting module (200) for a passenger service unit of an aircraft, comprising: a lighting source in a housing of the lighting module (200) for providing light and a gasper orifice in a housing of the gasper module (100) for supply of gasper air, wherein the lighting module (200) and the gasper module (100) are assembled in a housing assembly of the service device, wherein the housing assembly (300) is adapted to hold the lighting module (200) and the gasper module (100) essentially around an axis (Z) of the housing assembly. According to the invention the lighting module (200) and the gasper module (100) are separated to each other by a housing assembly bearing part (330), and a force transmission is applicable to the lighting module (200) and the gasper module (100) for independent movement of at least one of the lighting module (200) and the gasper module (100) relative to the bearing part (330), and wherein the gasper module housing (110) and the lighting module housing (210) are separately form fitted to the bearing part (330) by a positive locking, in particular wherein the positive locking as such is accomplished without any additional fixing elements.
摘要翻译：本发明涉及一种服务设备（1000），其具有用于飞机的乘客服务单元的气体模块（100）和照明模块（200）的系统，包括：照明模块（200）的壳体中的照明源），用于在用于提供气体空气的气体加热器模块（100）的壳体中提供光和气塞孔，其中所述照明模块（200）和所述吸气模块（100）组装在所述服务装置的壳体组件中，其中壳体组件（300）适于基本上围绕壳体组件的轴线（Z）保持照明模块（200）和吸气模块（100）。根据本发明，照明模块（200）和吸气模块（100）通过壳体组件支撑部分（330）彼此分离，并且力传递可应用于照明模块（200）和气体模块（ 100），用于相对于所述轴承部分（330）至少一个所述照明模块（200）和所述吸气模块（100）的独立移动，并且其中所述气体模块壳体（110）和所述照明模块壳体（210）是分开地通过正锁定装配到轴承部分（330）上，特别地，其中正锁定是这样实现的，而没有任何附加的固定元件。

3. 发明申请

US20140003073A1 Passenger service unit comprising a ventilaton nozzle and a reading light 审中-公开
标题翻译：乘客服务单元包括通风喷嘴和阅读灯
公开(公告)号：US20140003073A1
公开(公告)日：2014-01-02
申请号：US13929822
申请日：2013-06-28
申请人： INTERTECHNIQUE
发明人： Wolfgang Rittner , Günter Boomgaarden , Marco Hollm , Rüdiger Meckers , Hasso Weinmann
IPC分类号： B64D47/02
CPC分类号： A62B7/08 , A61M16/20 , A62B7/00 , A62B7/02 , A62B7/14 , A62B9/02 , A62B18/02 , A62B21/00 , B64D10/00 , B64D11/0015 , B64D11/00155 , B64D2231/00 , B64D2231/02 , C01B13/02 , C01B13/0296 , G08B5/00 , G08B5/224 , G08B5/36
摘要： The invention relates to a passenger service unit comprising a reading light and a ventilation nozzle. The ventilation nozzle is pivotably mounted within a frame wherein the frame is fixed to the passenger service unit. A ring shape-element is arranged circumferentially around the ventilation nozzle and incorporates a plurality of light means providing a light beam to the passenger. The light means are adjusted by an adjustment means which effects a relative movement of the light means to the ring-shaped element. The ring-shaped element is immovable fixed to the frame.
摘要翻译：本发明涉及一种乘客服务单元，包括阅读灯和通风喷嘴。通风喷嘴可枢转地安装在框架内，其中框架被固定到乘客服务单元。环状元件围绕通气喷嘴周向地布置并且包括向乘客提供光束的多个光装置。光装置通过调节装置进行调节，该调节装置实现光装置相对于环形元件的相对移动。环形元件固定在框架上。

4. 发明申请

US20140001062A1 Container for an oxygen supply unit, device and system of an arrangement of a number of oxygen supply devices, wherein each oxygen supply unit is stored in a container, method of control of a status and/or change of status of a container 有权
标题翻译：用于供氧单元的容器，多个供氧装置的装置的装置和系统，其中每个氧气供应单元存储在容器中，控制容器状态和/或状态变化的方法
公开(公告)号：US20140001062A1
公开(公告)日：2014-01-02
申请号：US13893511
申请日：2013-05-14
申请人： INTERTECHNIQUE
发明人： Marco Hollm , Hasso Weinmann , Gunter Boomgarden , Mark Niedostatek , Rudiger Meckes , Wolfgang Rittner
IPC分类号： B64D13/00
CPC分类号： B64D13/00 , A62B25/005 , B64D11/00 , B64D2231/025
摘要： The invention relates to a container for an oxygen supply unit, having a container well at least, wherein a container door can be pivotably joint at a container well's edge, wherein the container is provided with a sensor system, adapted to indicate a status and/or change of status of the door, in particular relative to the well. The invention further relates to a system of an arrangement of a number of oxygen supply devices of claim 11 in a ceiling-panel along an aircrafts cabin, in particular along an aircrafts cabin alley of seats, wherein each oxygen supply unit is stored in a container, in particular in a container according to one of claims 1 to 10.
摘要翻译：本发明涉及一种用于供氧单元的容器，其至少具有容器，其中容器门可以在容器井的边缘处可枢转地接合，其中容器设置有传感器系统，适于指示状态和/ 或更改门的状态，特别是相对于井。本发明还涉及一种如权利要求11所述的多个供氧装置的装置的系统，其特征在于沿着飞机机舱的天花板板，特别是沿着座椅的飞机机舱小巷，其中每个供氧单元被储存在容器，特别是在根据权利要求1至10中任一项所述的容器中。

5. 发明授权

US09656106B2 Aircraft oxygen emergency apparatus with quick release box 有权
公开(公告)号：US09656106B2
公开(公告)日：2017-05-23
申请号：US13928455
申请日：2013-06-27
申请人： INTERTECHNIQUE
发明人： Marco Hollm , Hasso Weinmann , Andreas Westphal , Wolfgang Rittner , Rüdiger Meckes , Frederik Hoffmann , Romain Ducos , Günter Boomgaarden , Benjamin Fleczok
IPC分类号： A62B18/08 , A62B25/00 , A62B7/14
CPC分类号： A62B25/005 , A62B7/14
摘要： The invention relates to an emergency oxygen supply device for aircraft inhabitants, comprising a container, wherein an oxygen mask is positioned inside said container, a releasable cover and a latch mechanism comprising a latch locking said cover lid. According to the invention said latch mechanism comprises a permanent magnet interacting with a magnetisable element an exerting a magnetic holding force onto said magnetisable element to hold said latch in a locking position, wherein a solenoid is positioned adjacent to the permanent magnet, said solenoid being connected to a control unit said control unit being adapted to receive an opening signal and to provide a current flowing through said solenoid in response to such opening signal, wherein said solenoid is arranged and dimensioned such that the current flowing through said solenoid reduces said magnetic holding force to such a level that the latch is released in a n unlocking position.

6. 发明申请

US20150000668A1 Aircraft oxygen emergency apparatus with quick release box 有权
标题翻译：具有快速释放箱的飞机氧气应急装置
公开(公告)号：US20150000668A1
公开(公告)日：2015-01-01
申请号：US13928455
申请日：2013-06-27
申请人： Intertechnique
发明人： Marco Hollm , Hasso Weinmann , Andreas Westphal , Wolfgang Rittner , Rüdiger Meckes , Frederik Hoffman , Romain Ducos , Günter Boomgaarden , Benjamin Fleczok
IPC分类号： A62B25/00 , A62B7/14 , A62B18/02
CPC分类号： A62B25/005 , A62B7/14
摘要： The invention relates to an emergency oxygen supply device for aircraft inhabitants, comprising a container, wherein an oxygen mask is positioned inside said container, a releasable cover and a latch mechanism comprising a latch locking said cover lid. According to the invention said latch mechanism comprises a permanent magnet interacting with a magnetisable element an exerting a magnetic holding force onto said magnetisable element to hold said latch in a locking position, wherein a solenoid is positioned adjacent to the permanent magnet, said solenoid being connected to a control unit said control unit being adapted to receive an opening signal and to provide a current flowing through said solenoid in response to such opening signal, wherein said solenoid is arranged and dimensioned such that the current flowing through said solenoid reduces said magnetic holding force to such a level that the latch is released in a n unlocking position.
摘要翻译：本发明涉及一种用于飞行器居民的紧急供氧装置，包括容器，其中氧气面罩位于所述容器内部，可释放盖和闩锁机构，其包括锁定所述盖盖的闩锁。根据本发明，所述闩锁机构包括与可磁化元件相互作用的永磁体，其向所述可磁化元件施加磁力保持力以将所述闩锁保持在锁定位置，其中螺线管与所述永磁体相邻地定位，所述螺线管被连接控制单元，所述控制单元适于接收打开信号并响应于这种打开信号提供流过所述螺线管的电流，其中所述螺线管的布置和尺寸使得流过所述螺线管的电流减小所述磁力保持力达到使闩锁释放在解锁位置的水平。

7. 发明申请

US20140000591A1 Emergency oxygen device, oxygen supply system and method for activating an emergency oxygen device for at least one passenger of an aircraft 审中-公开
标题翻译：紧急氧气装置，氧气供应系统和用于激活飞机至少一名乘客的紧急氧气装置的方法
公开(公告)号：US20140000591A1
公开(公告)日：2014-01-02
申请号：US13914757
申请日：2013-06-11
申请人： INTERTECHNIQUE
发明人： Marco Hollm , Hasso Weinmann , Gunter Boomgarden , Mark Niedostatek , Rudiger Meckes , Wolfgang Rittner
IPC分类号： A62B7/14 , A62B18/02 , A62B7/08
CPC分类号： A62B7/14 , A62B7/08 , A62B9/02 , A62B18/02 , A62B18/10
摘要： The invention relates to an emergency oxygen device for at least one passenger of an aircraft, comprising a chemical oxygen generator and/or oxygen pressure cylinder including an oxygen source and a starter unit adapted for initiating a reaction in said oxygen source producing oxygen, at least one oxygen mask each connected with the oxygen source such that an oxygen fluid flow from said oxygen source after said starter unit has initiated the reaction is receivable at the oxygen mask, an activation assembly for activating the starter unit, and whereby the activation assembly comprises an actuator assembly comprising a shape memory material based actuator.
摘要翻译：本发明涉及一种用于飞机的至少一名乘客的紧急氧气装置，其包括化学氧气发生器和/或氧气压力缸，所述氧气发生器和/或氧气压力缸包括氧源和适于在所述氧源中引发产生氧的反应的起动器单元，至少一个氧气掩模，每个与氧源连接，使得在所述启动器单元已启动反应之后来自所述氧源的氧流体流动在氧气掩模处接收，用于激活起动器单元的激活组件，并且由此激活组件包括致动器组件包括基于形状记忆材料的致动器。

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