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公开(公告)号：US10071816B2
公开(公告)日：2018-09-11
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.
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公开(公告)号：US09718531B2
公开(公告)日：2017-08-01
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.
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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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