OXYGEN BREATHING MASK
    11.
    发明申请
    OXYGEN BREATHING MASK 失效
    氧气呼吸面罩

    公开(公告)号:US20100000536A1

    公开(公告)日:2010-01-07

    申请号:US12475795

    申请日:2009-06-01

    IPC分类号: A62B9/02 A62B18/02

    CPC分类号: A62B7/14 B64D2231/025

    摘要: Oxygen breathing masks, as well as methods of providing oxygen to persons, are detailed. The devices may include mechanisms for supplying either oxygen or ambient air to a person depending on inspiration pressure applied by the person to a first volume to which the person's mouth and/or nose is connected.

    摘要翻译: 详细说明了氧气呼吸面罩,以及向人员提供氧气的方法。 所述装置可以包括用于根据由人施加到人口和/或鼻子所连接的第一体积的吸气压力向人提供氧气或环境空气的机构。

    EMERGENCY OXYGEN SYSTEM FOR AIRCRAFT PASSENGERS
    12.
    发明申请
    EMERGENCY OXYGEN SYSTEM FOR AIRCRAFT PASSENGERS 有权
    飞机乘客紧急氧气系统

    公开(公告)号:US20090014003A1

    公开(公告)日:2009-01-15

    申请号:US11318991

    申请日:2005-12-27

    IPC分类号: A61M16/06

    摘要: An emergency oxygen system is provided for aircraft passengers. The system includes at least one oxygen mask (2), with a sensor (4) for detecting at least one breathing characteristic value of a passenger using this oxygen mask (2). A control unit (10) individually determines the oxygen requirement of the passenger on account of the detected breathing characteristic value. A dosing device (8) is actuated by the control unit (10). The dosing device (8) supplies an oxygen quantity corresponding to the determined oxygen requirement, to the oxygen mask (2).

    摘要翻译: 为飞机乘客提供紧急氧气系统。 该系统包括至少一个氧气面罩(2),其具有用于使用该氧气面罩(2)检测乘客的至少一个呼吸特征值的传感器(4)。 控制单元(10)根据检测到的呼吸特性值分别确定乘客的氧气需求量。 计量装置(8)由控制单元(10)致动。 给药装置(8)将对应于所确定的氧需求的氧量提供给氧气面罩(2)。

    Regulation valve for a life support system
    13.
    发明授权
    Regulation valve for a life support system 有权
    生命维持系统调节阀

    公开(公告)号:US09016278B2

    公开(公告)日:2015-04-28

    申请号:US13189701

    申请日:2011-07-25

    摘要: There is provided a regulation valve for a life support system for use in an aircraft cabin. The valve may have a gas inlet, an air mask supply outlet connected to the gas inlet, and a pressure vest branch interconnected between the gas inlet and an opening. The valve may further have a decompression valve adapted to inhibit gas flow from the pressure vest branch to the air mask supply outlet if pressure in the aircraft cabin decreases below a predetermined value, a one-way valve adapted to inhibit gas flow from the pressure vest branch to the air mask supply outlet at a predetermined pressure difference between the pressure vest branch and the gas inlet, and a one-way dump valve adapted to direct gas from the pressure vest branch to the environment at the predetermined pressure difference between the pressure vest branch and the gas inlet.

    摘要翻译: 提供了一种用于飞机机舱中的生命支持系统的调节阀。 阀可以具有气体入口,连接到气体入口的空气掩模供给出口和在气体入口和开口之间互连的压力背心分支。 阀还可以具有减压阀,该减压阀适用于如果飞行器舱内的压力降低到预定值以下,则抑制气体从压力背心分支到气罩供应出口的流动,适用于抑制来自压力背心的气体流动的单向阀 以压力背心分支和气体入口之间的预定压力差分配到防毒面具供应出口,以及单向排放阀,其适于将压力背心支管的气体以压力背心之间的预定压力差引导到环境 分支和气体入口。

    Passenger cabin emergency oxygen device
    14.
    发明授权
    Passenger cabin emergency oxygen device 有权
    客舱应急氧气装置

    公开(公告)号:US08882033B2

    公开(公告)日:2014-11-11

    申请号:US13363531

    申请日:2012-02-01

    IPC分类号: B64D11/00 A62B7/14

    CPC分类号: A62B7/14 B64D11/00 Y02T50/46

    摘要: The Invention relates to a passenger cabin emergency oxygen device for an aircraft, comprising at least one electrically driven activation device for activating the emergency oxygen device, at least one energy storage device and a source of electrical energy. Said source of electrical energy and said energy storage device are coupled together for substantially constant energy transmission from the source of electrical energy to the energy storage device at a first energy level, an activation device and a controller are coupled together for signal transmission from the controller to the activation device, said activation device and said energy storage device are coupled together for energy transmission from the energy storage device to the activation device at a second energy level which is higher than the first energy level.

    摘要翻译: 本发明涉及一种用于飞机的客舱应急氧气装置,包括至少一个用于启动紧急氧气装置的电驱动致动装置,至少一个储能装置和电能源。 所述电能源和所述能量存储装置耦合在一起,以在第一能级从电能源到能量存储装置的能量传输基本上恒定,激活装置和控制器耦合在一起,以便从控制器传送信号 所述激活装置和所述能量存储装置耦合在一起,以便在高于第一能量级的第二能级从能量存储装置到激活装置的能量传输。

    Oxygen breathing mask
    15.
    发明授权
    Oxygen breathing mask 失效
    氧气呼吸面罩

    公开(公告)号:US08474456B2

    公开(公告)日:2013-07-02

    申请号:US12475795

    申请日:2009-06-01

    IPC分类号: A62B7/04 F16K31/26

    CPC分类号: A62B7/14 B64D2231/025

    摘要: Oxygen breathing masks, as well as methods of providing oxygen to persons, are detailed. The devices may include mechanisms for supplying either oxygen or ambient air to a person depending on inspiration pressure applied by the person to a first volume to which the person's mouth and/or nose is connected.

    摘要翻译: 详细说明了氧气呼吸面罩,以及向人员提供氧气的方法。 所述装置可以包括用于根据由人施加到人口和/或鼻子所连接的第一体积的吸气压力向人提供氧气或环境空气的机构。

    Oxygen emergency supply device
    16.
    发明申请
    Oxygen emergency supply device 有权
    氧气应急供应装置

    公开(公告)号:US20070283960A1

    公开(公告)日:2007-12-13

    申请号:US11809037

    申请日:2007-05-31

    IPC分类号: A61M16/00 A62B9/02

    摘要: An oxygen emergency supply device for an aircraft includes an oxygen pressure vessel, which is in fluid connection with at least one oxygen mask. Means for closing and opening the oxygen pressure vessel, means for pressure reduction, a pressure regulation device, and a flow throttle are provided in the conduit connection between the oxygen pressure vessel and the oxygen mask. The oxygen emergency supply device further includes a control device. A controllable shut-off valve forms the means for closing and opening the oxygen pressure vessel, the means for pressure reduction and a part of the pressure regulation device.

    摘要翻译: 用于飞机的氧气应急供应装置包括与至少一个氧气面罩流体连接的氧气压力容器。 在氧气压力容器和氧气面罩之间的管道连接中设置用于关闭和打开氧气压力容器的装置,用于减压的装置,压力调节装置和流量节流阀。 氧气应急供给装置还包括控制装置。 可控截止阀形成用于关闭和打开氧气压力容器,减压装置和压力调节装置的一部分的装置。

    Passenger oxygen mask
    17.
    发明申请
    Passenger oxygen mask 审中-公开
    乘客氧气面罩

    公开(公告)号:US20050284480A1

    公开(公告)日:2005-12-29

    申请号:US11159030

    申请日:2005-06-22

    IPC分类号: A62B18/08 B64D11/00 A62B18/02

    摘要: A passenger oxygen mask for an aircraft with a mask body which is to come to bear on the face in a use situation and which engages over of the mouth and nose in the correct position of use. A lead-through for a drinking tube is provided.

    摘要翻译: 用于具有面罩体的飞行器的乘客氧气面罩,其将在使用状况下承受在脸上,并且在正确的使用位置上接合口和鼻部。 提供了一种用于饮用管的通孔。

    Chemical oxygen generator with core channel tube for an emergency oxygen device
    18.
    发明授权
    Chemical oxygen generator with core channel tube for an emergency oxygen device 有权
    化学氧气发生器与核心通道管用于紧急氧气装置

    公开(公告)号:US09108074B2

    公开(公告)日:2015-08-18

    申请号:US13358611

    申请日:2012-01-26

    摘要: Embodiments of the invention relate to a chemical oxygen generator for an emergency oxygen device, comprising an outer housing defining an interior space and comprising an outlet opening, a solid oxygen source within said interior space containing a material which is able to produce oxygen in a chemical reaction. According to embodiments of the invention, a hollow tube within said interior space is embedded in said solid oxygen source.

    摘要翻译: 本发明的实施例涉及一种用于紧急氧气装置的化学氧气发生器,包括限定内部空间并包括出口开口的外壳体,所述内部空间内的固体氧源包含能够在化学品中产生氧的材料 反应。 根据本发明的实施例,所述内部空间中的中空管嵌入所述固体氧源中。

    Oxygen breathing device for an aircraft
    19.
    发明授权
    Oxygen breathing device for an aircraft 有权
    用于飞机的氧气呼吸装置

    公开(公告)号:US08171932B2

    公开(公告)日:2012-05-08

    申请号:US12501525

    申请日:2009-07-13

    CPC分类号: A62B7/14 A62B7/08 A62B7/10

    摘要: The invention relates to an oxygen breathing device for an aircraft, in particular for oxygen supply to crew member in a cockpit of an aircraft, comprising a filter unit having an inflow port and an outflow port, the filter unit being adapted to extract nitrogen from an air flow flowing from the inflow port to the outflow port through the filter unit, wherein the filter unit is adapted to receive compressed air, preferably, bleed air from a precompressor stage of a turbine driving the aircraft, or directly by a separate electrically driven compressor, via a bleed air supply line connected to the inflow port, a first pressure regulator in the bleed air supply line, a first water separator which is arranged in the bleed air supply line in flow direction of the bleed air before the first pressure regulator and a connection port which can be brought in fluid communication with said outflow port of the filter unit and which is adapted to be coupled to at least one oxygen supply mask via an oxygen supply line. According to the invention, a chemical oxygen generator comprising at least one substance adapted to produce oxygen in a chemical reaction and to provide said oxygen to an outflow port of said oxygen generator is provided. The outflow port of said chemical oxygen generator is connected to an auxiliary oxygen supply line and a control unit is adapted to selectively provide oxygen from the filter unit or the chemical oxygen generator to an oxygen supply mask coupled to the connection port.

    摘要翻译: 本发明涉及一种用于飞行器的氧呼吸装置,特别是用于向飞行器驾驶舱中的乘务员供氧的供氧装置,其包括具有入口和流出口的过滤单元,该过滤单元适于从 空气流通过过滤器单元从流入口流到流出口,其中过滤器单元适于接收压缩空气,优选地,从驱动飞行器的涡轮机的预压缩器级排放空气,或直接由单独的电动压缩机 通过连接到流入口的排气供应管线,在排气供应管线中的第一压力调节器,在第一压力调节器之前在排气的流动方向上布置在排气供应管路中的第一水分离器,以及 连接端口,其可以与过滤器单元的所述流出端口流体连通,并且适于经由至少一个氧气供给掩模经由 供氧线。 根据本发明,提供一种化学氧发生器,其包括适于在化学反应中产生氧并将氧提供给所述氧气发生器的流出口的至少一种物质。 所述化学氧气发生器的流出口连接到辅助氧供应管线,并且控制单元适于从过滤器单元或化学氧气发生器选择性地提供氧气到耦合到连接端口的氧气供给掩模。

    AIR EXIT GUIDANCE
    20.
    发明申请
    AIR EXIT GUIDANCE 有权
    空运指导

    公开(公告)号:US20070042701A1

    公开(公告)日:2007-02-22

    申请号:US11465649

    申请日:2006-08-18

    IPC分类号: B60H1/30

    摘要: An air exit guidance which in particular is provided for arrangement in the personal service unit of an passenger aircraft. The guidance includes an air inlet and an air outlet as well as an adjustable throttle which is arranged at the inflow side of the air exit guidance.

    摘要翻译: 特别提供用于在客机的个人服务单元中安排的排气引导件。 引导件包括进气口和出气口以及布置在出气引导件的流入侧的可调节节流阀。