-
21.发明申请公开(公告)号：US20140048649A1
公开(公告)日：2014-02-20
申请号：US13966347
申请日：2013-08-14
申请人： INTERTECHNIQUE
摘要： Embodiments of the present invention provide improved space utilization concepts for aircraft, and particularly to using under floor space created by the envelope designed to house an airstair system. For example, this space may be used to house and integrate one or more fuel cell system(s) and/or components, such as hydrogen tanks and/or the fuel cell body, such that the fuel cell system can deliver useful byproducts to support various aircraft functions. Additionally or alternatively, the space may be used to store other components.
摘要翻译： 本发明的实施例为飞行器提供了改进的空间利用概念，特别是使用由设计成容纳一个空降机系统的外壳产生的底板空间。 例如，该空间可以用于容纳和集成一个或多个燃料电池系统和/或组件，例如氢气罐和/或燃料电池体，使得燃料电池系统可以递送有用的副产物以支持 各种飞机功能。 另外或替代地，空间可以用于存储其他部件。
-
公开(公告)号：US20130277501A1
公开(公告)日：2013-10-24
申请号：US13834964
申请日：2013-03-15
申请人： INTERTECHNIQUE
发明人： JULIEN DELRIEU
IPC分类号： B64D15/16
CPC分类号： B64D15/16
摘要： An de-icing system comprising a shield that is configured to deform in a pre-determined way that de-bonds accreted ice. In some embodiments, the shield has a variable (non-uniform) stiffness across its width and/or length such that it undergoes a twist-like or other suitable deformation when subjected to a force. In some embodiments, the system includes a plurality of electro-mechanical actuators configured to generate the force applied to the shield.
摘要翻译： 一种除冰系统，其包括被配置成以预定的方式变形以使去除冰的冰块的屏蔽。 在一些实施例中，屏蔽件在其宽度和/或长度上具有可变（非均匀）刚度，使得其在受到力时经历扭曲状或其它合适的变形。 在一些实施例中，该系统包括被配置为产生施加到屏蔽的力的多个机电致动器。
-
公开(公告)号：US20130247913A1
公开(公告)日：2013-09-26
申请号：US13895879
申请日：2013-05-16
申请人： INTERTECHNIQUE
发明人： SÉVERINE AUBONNET , VINCENT GRETER
摘要： The invention relates to a respiratory gas supply circuit for an aircraft carrying passengers, comprising a pressurized source of respiratory gas (R1, R2) and a supply line (2, 3), said circuit further comprising on said supply line a regulating device (12, 30) for controlling the supply in respiratory gas to said passengers, wherein said regulating device further comprises an electro-valve (12) controlled by a pulse width modulation signal provided by an electronic unit (20).
-
公开(公告)号：US20130134334A1
公开(公告)日：2013-05-30
申请号：US13700138
申请日：2010-06-01
申请人： Frederic Denat , Mourad Rezig
发明人： Frederic Denat , Mourad Rezig
IPC分类号： F16K31/00
CPC分类号： F16K31/00 , F16K31/043 , F16K31/046 , F16K37/0083 , F16K37/0091
摘要： The valve actuator (1) includes a housing (2), a motor (4) coupled to the valve, wherein rotation of the motor (4) changes the position of the valve from a first position in which fluid flow may occur along at least one path and a second position in which fluid flow is either blocked or may occur along at least one second path, said motor (4) being normally supplied with electrical power from a main source of electrical power, at least one sensor (24,132) configured to detect the position of the valve and/or the valve speed, a switch (16) controlling the delivery of electrical power to the motor (4), and a power circuitry (19) connected to the switch (16). The valve actuator further includes a controller (20) connected to the at least one sensor (24,132) and to the power circuitry (19), said controller (20) collecting in real time data relative to the position and/or the speed of the valve and data relative to the power setting, calculating the position and/or speed correction in pro rata to errors between the collected data relative to the position and/or the speed of the valve and collected data relative to the power setting, and sending a new power setting to the power circuitry (19), wherein the power circuitry (19) amplifies the controller signal.
摘要翻译： 阀致动器（1）包括壳体（2），联接到阀的马达（4），其中马达（4）的旋转使阀的位置从至少可能发生流体流动的第一位置改变 一个路径和第二位置，其中流体流被阻挡或沿着至少一个第二路径可能发生，所述马达（4）通常从主电源供应电力，至少一个传感器（24,132）被配置 检测阀的位置和/或阀速度，控制向电动机（4）的电力输送的开关（16）以及连接到开关（16）的电力电路（19）。 所述阀致动器还包括连接到所述至少一个传感器（24,132）和所述电源电路（19）的控制器（20），所述控制器（20）相对于所述至少一个传感器的位置和/或速度实时收集数据 阀门和相对于功率设置的数据，根据收集的数据相对于阀的位置和/或速度和相对于功率设置的收集数据之间的误差计算位置和/或速度校正，并发送 电力电路（19）的新功率设置，其中电源电路（19）放大控制器信号。
-
公开(公告)号：US20130037031A1
公开(公告)日：2013-02-14
申请号：US13641872
申请日：2010-08-02
申请人： Simon Gredat
发明人： Simon Gredat
IPC分类号： A62B18/08
CPC分类号： A62B18/084 , F16L11/121
摘要： A tube (23) for inflatable harness (1) of a breathing mask (3), the tube (23) is gas impermeable, supple and has an inner surface (22) and an outer surface (24), wherein the inner surface (22) of the tube (23) includes a plurality of protrusions (30).
摘要翻译： 一种用于呼吸面罩（3）的充气线束（1）的管（23），所述管（23）是不透气的，柔软的并且具有内表面（22）和外表面（24），其中内表面 管（23）的内表面（22）包括多个突起（30）。
-
公开(公告)号：US20130037029A1
公开(公告)日：2013-02-14
申请号：US13606076
申请日：2012-09-07
CPC分类号： A62B7/14 , A62B7/02 , A62B7/08 , A62B9/00 , Y10T29/49769 , Y10T29/49826
摘要： The invention relates to an arrangement of a plurality of oxygen breathing devices, in particular for providing oxygen to passenger or crew of an aircraft, each oxygen breathing device comprising an oxygen source, wherein oxygen is stored, in particular in chemically bound form or compressed form, an oxygen guiding device for guiding oxygen from the oxygen source to a person. According to the invention, an arrangement of a plurality of oxygen breathing devices is provided, wherein a first one of said plurality of oxygen breathing devices further comprises an integrated transmitter comprising a sender adapted for wireless communication with a receiver of a second one of said oxygen breathing devices and a receiver adapted for wireless communication with a sender of said second oxygen breathing device.
摘要翻译： 本发明涉及多个氧呼吸装置的布置，特别是为飞机的乘客或乘员提供氧气，每个氧气呼吸装置包括氧源，其中氧被储存，特别是化学结合形式或压缩形式 ，用于将氧气从氧源引导到人的氧气引导装置。 根据本发明，提供了多个氧呼吸装置的布置，其中所述多个氧呼吸装置中的第一个氧气呼吸装置还包括集成发射器，其包括适于与所述氧气中的第二个氧接收器的接收器无线通信的发射器 呼吸装置和适于与所述第二氧呼吸装置的发送器无线通信的接收器。
-
公开(公告)号：US08261744B2
公开(公告)日：2012-09-11
申请号：US12538185
申请日：2009-08-10
CPC分类号： A62B7/14 , A62B7/02 , A62B7/08 , A62B9/00 , Y10T29/49769 , Y10T29/49826
摘要： The invention relates to an arrangement of a plurality of oxygen breathing devices, in particular for providing oxygen to passenger or crew of an aircraft, each oxygen breathing device comprising an oxygen source, wherein oxygen is stored, in particular in chemically bound form or compressed form, an oxygen guiding device for guiding oxygen from the oxygen source to a person. According to the invention, an arrangement of a plurality of oxygen breathing devices is provided, wherein a first one of said plurality of oxygen breathing devices further comprises an integrated transmitter comprising a sender adapted for wireless communication with a receiver of a second one of said oxygen breathing devices and a receiver adapted for wireless communication with a sender of said second oxygen breathing device, wherein said second oxygen breathing device is arranged in a distance from the first oxygen breathing device, wherein the sender and receiver of said integrated transmitter are adapted to receive and send at least a decompression signal signalising the need to activate oxygen supply from said oxygen source via said oxygen guiding device, and wherein preferably said transmitter is connected to said oxygen source to activate oxygen supply via said oxygen guiding device upon receipt of such decompression signal.
摘要翻译： 本发明涉及多个氧呼吸装置的布置，特别是为飞机的乘客或乘员提供氧气，每个氧气呼吸装置包括氧源，其中氧被储存，特别是化学结合形式或压缩形式 ，用于将氧气从氧源引导到人的氧气引导装置。 根据本发明，提供了多个氧呼吸装置的布置，其中所述多个氧呼吸装置中的第一个氧气呼吸装置还包括集成发射器，其包括适于与所述氧气中的第二个氧接收器的接收器无线通信的发射器 呼吸装置和适于与所述第二氧气呼吸装置的发送器进行无线通信的接收器，其中所述第二氧气呼吸装置布置在距离所述第一氧气呼吸装置一定距离的位置，其中所述集成发射器的发射器和接收器适于接收 并且发送至少一个减压信号，其指示需要通过所述氧气引导装置从所述氧源激活氧供应，并且其中优选地，所述发射器连接到所述氧源，以在接收到所述减压信号时通过所述氧气引导装置激活供氧 。
-
公开(公告)号：US08171932B2
公开(公告)日：2012-05-08
申请号：US12501525
申请日：2009-07-13
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。
-
29.发明授权Breathing gas feed assembly for aircraft flight crew, and a stowage box for an emergency breathing mask 有权用于飞机机组人员的呼吸气体馈送组件和用于紧急呼吸面罩的收纳箱公开(公告)号：US07343918B2
公开(公告)日：2008-03-18
申请号：US10716970
申请日：2003-11-18
CPC分类号： A62B25/005 , B64D2231/025
摘要： A breathing gas feed assembly for the flight crew of an airplane comprises an emergency breathing mask and a stowage box for the mask. The box is adapted to receive the mask diagonally and it is closed by two doors hinged about respective hinge axes situated on two adjacent edges of the box.
摘要翻译： 用于飞机机组人员的呼吸气体馈送组件包括紧急呼吸面罩和用于面罩的收纳箱。 盒子适于对角地接收掩模，并且由铰接在位于盒的两个相邻边缘上的相应铰链轴的两个门封闭。
-
30.发明授权公开(公告)号：US07082946B2
公开(公告)日：2006-08-01
申请号：US10284714
申请日：2002-10-31
申请人： Eric Farin , Michel Bardel , Nicolas Bloch
发明人： Eric Farin , Michel Bardel , Nicolas Bloch
IPC分类号： A62B18/02
CPC分类号： A62B7/14
摘要： In order to protect the passengers of an airplane against the effects of depressurization of the cabin, breathing masks are fed with oxygen at a rate which is an increasing function of cabin altitude. Oxygen is fed via a constriction and an economizer bag, and an initial fraction only of the gases breathed out is caused to be re-breathed by collecting the initial fraction in a flexible re-breathing bag in communication with the mask. The re-breathing bag has a volume in inflated state which is not less than the total dead volume of the respiratory tract and the mask. A protective apparatus comprises a feed control unit supplying an adjustable flow rate to masks connected to a general pipe via respective economizer bags. A re-breathing bag retards re-breathing and stores only an initial fraction of the gases breathed out on each exhalation.
摘要翻译： 为了保护飞机的乘客不受舱室减压的影响，呼吸面罩以一个增加舱室高度的功能的速度供给氧气。 通过收缩和节约器袋供给氧气，并且通过在与面罩连通的柔性再呼吸袋中收集初始分数，仅引起呼出气体的初始部分被再次呼吸。 再呼吸袋体积处于膨胀状态，不小于呼吸道和面罩的总死体积。 保护装置包括供给控制单元，该供给控制单元通过相应的经济器袋向与通用管连接的面罩提供可调节流量。 再呼吸袋延迟呼吸，并且仅存储每次呼气时呼出的气体的初始部分。
-
-
-
-
-
-
-
-
-
搜索结果
113 条记录 (耗时 0.019 秒)
