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公开(公告)号：US20160009361A1
公开(公告)日：2016-01-14
申请号：US14772429
申请日：2014-02-26
摘要： A system for shielding of at least one component (28) within an aircraft (10) includes a floor panel disposed at least partially between joists (38) supporting a floor (30) within the aircraft and a ground plane (44) connected to a bottom surface of the floor panel. The ground plane extends at least partially between adjacent joists. At least one bracket (52) electrically connects the ground plane to at least one of the joists.
摘要翻译： 用于遮蔽飞行器（10）内的至少一个部件（28）的系统包括至少部分地布置在支撑飞机内的地板（30）的托梁（38）之间的底板和连接到飞机 底板底面。 接地平面至少部分延伸在相邻的托梁之间。 至少一个托架（52）将接地平面电连接到至少一个托梁。
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公开(公告)号：US20180286531A1
公开(公告)日：2018-10-04
申请号：US15736571
申请日：2016-06-17
申请人： BOMBARDIER INC.
CPC分类号： H01B7/009 , B60R16/0207 , B64D47/00 , B64D2221/00 , F16D66/00 , H01B7/0045 , H01R24/28
摘要： There is described herein a harness (106) that remains neutral until configured by a configuration device (110). Wires that connect to specific pins responsible for the configuration of a system are taken out and connected to a configuration port (108) on the harness (106). The configuration port (108), when mated with the configuration device (110), sets a configuration setting of the system. The configuration device (110) may be used to set the power and/or signal parameters of the harness (106) for a system or to configure various options within the system itself or another system.
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公开(公告)号：US20170001731A1
公开(公告)日：2017-01-05
申请号：US14769889
申请日：2014-03-06
申请人： BOMBARDIER INC.
CPC分类号： B64D37/32 , B64D37/005 , B64D37/02
摘要： A tank wall connector system for use with a composite tank, the connector comprises a connector having a body extending from an interior of the tank to an exterior of the tank when installed through a hole in the composite tank. The connector has a first electrical conductivity property. An interface is positioned between the connector and a wall of the composite tank when installed to the tank thereby preventing physical contact between the connector and the tank wall in the interior of the tank, the interface having a second electrical conductivity property, different from the first electrical conductivity property.
摘要翻译： 一种与复合罐一起使用的罐壁连接器系统，连接器包括连接器，当通过复合罐中的孔安装时，该连接器具有从罐的内部延伸到罐的外部的主体。 连接器具有第一导电性。 当连接器和复合罐的壁安装在罐上时，接口被定位在复合罐的壁之间，从而防止连接器与罐内部的罐壁之间的物理接触，该界面具有第二导电性，不同于第一 导电性能。
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4.发明申请INTERFACE BETWEEN FIRE SUPPRESSANT CONDUIT AND CARGO COMPARTMENT OF AN AIRCRAFT 审中-公开消防队员与飞机货舱之间的接口公开(公告)号：US20160008641A1
公开(公告)日：2016-01-14
申请号：US14771924
申请日：2014-02-24
申请人： BOMBARDIER INC.
CPC分类号： A62C3/08 , A62C35/68 , B64D45/00 , B64D2045/009
摘要： Apparatus and methods related to fire suppression in cargo compartments of aircraft are disclosed. An exemplary apparatus provides an interface (38) between a fire suppressant conduit (18) and a cargo panel (28) of a cargo compartment (12) of an aircraft (10). The apparatus comprises an adaptor (40) configured to provide the fire suppressant conduit (18) access to the cargo compartment (12) through the cargo panel (28) and a sealing member (42) configured to provide a seal between the adaptor (40) and the fire suppressant conduit (18). The adaptor (40) comprises an aperture (56) for receiving the fire suppressant conduit (18) where the aperture (56) is sized to permit passage of a nozzle (36) of the fire suppressant conduit (18) therethrough. Associated methods (600, 700) for removing the cargo panel (28) of the cargo compartment (12) of the aircraft (10) without disassembly of the nozzle (36) of the fire suppressant conduit (18) are also disclosed.
摘要翻译： 披露了与飞机货舱内的灭火有关的装置和方法。 示例性装置提供了消防管道（18）和飞机（10）的货舱（12）的货物面板（28）之间的接口（38）。 该装置包括适配器（40），其配置成提供消防管道（18）通过货物面板（28）进入货物舱（12）;以及密封构件（42），该密封构件构造成在适配器（40） ）和消防管道（18）。 适配器（40）包括用于接收消防管道（18）的孔口（56），其中孔口（56）的尺寸设置成允许消防管道（18）的喷嘴（36）通过其中。 还公开了用于移除飞行器（10）的货舱（12）的货物面板（28）而不拆卸消防管道（18）的喷嘴（36）的相关方法（600,700）。
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公开(公告)号：US20180141634A1
公开(公告)日：2018-05-24
申请号：US15874252
申请日：2018-01-18
申请人： BOMBARDIER INC.
摘要： A system for shielding of at least one component within an aircraft includes a floor panel disposed at least partially between joists supporting a floor within the aircraft and a ground plane connected to a bottom surface of the floor panel. The ground plane extends at least partially between adjacent joists. At least one bracket electrically connects the ground plane to at least one of the joists.
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公开(公告)号：US20160009358A1
公开(公告)日：2016-01-14
申请号：US14770588
申请日：2014-02-24
申请人： BOMBARDIER INC.
CPC分类号： B64C1/1453 , B64D41/00
摘要： A drain for expelling fluids from an interior of an aircraft to an exterior of the aircraft, the drain including a drain tube disposed at the interior of the aircraft having a first end disposed in fluid communication with an aircraft equipment to be drained and an opposite second end, wherein the drain tube terminates at the second end at a location within the interior of the aircraft, a seal which extends between the second end of the drain tube and an outer skin of the aircraft, delimiting a drainage cavity, and a drainage pathway extending from the cavity through the outer skin to the exterior of the aircraft.
摘要翻译： 用于将流体从飞行器的内部排出到飞行器的外部的排水口，排水口包括设置在飞行器内部的排水管，第一端设置成与待排水的飞机设备流体连通，并且相对的第二 其中所述排水管在所述第二端处终止于所述飞行器内部的位置处，所述密封件在所述排水管的所述第二端与所述飞行器的外皮之间延伸，限定排水腔，以及排出通道 从空腔延伸通过外皮到飞机的外部。
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