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公开(公告)号：US09233758B2
公开(公告)日：2016-01-12
申请号：US13327850
申请日：2011-12-16
IPC分类号： B64D37/32 , B64D45/02 , F16L13/02 , F16L13/10 , F16L25/01 , F16L25/02 , F16L25/03 , F16L47/03 , F16L47/24
CPC分类号： F16L39/005 , B64D37/32 , B64D45/02 , F16L13/0245 , F16L13/103 , F16L25/01 , F16L25/025 , F16L25/03 , F16L47/03 , F16L47/24 , Y02T50/44 , Y10T137/0402
摘要： A fuel line assembly for an aircraft comprises a ferrule assembly comprising a ferrule affixed to an isolation tube, which may be directly affixed to a fuel tube or affixed to an extension tube, which in turn, is affixed to the fuel tube. The ferrule assembly provides electrostatic discharge protection and lightning protection as the isolation tube maintains a separation distance from the ferrule and fuel tube, both of which are made from metal. The isolation tube is made from a dielectric material, but which may have conductive particles added to aid in the dissipation of an electrostatic charge. The electrical resistance through the isolation tube has a lower limit to arrest the flow of the induced lightning current through the assembly. The amount of lightning protection afforded can be configured. The ferrule assembly components may be affixed by using thermo-welding, adhesive, or mechanical pressure.
摘要翻译： 用于飞行器的燃料管线组件包括套圈组件，其包括固定到隔离管的套圈，所述套圈可以直接固定到燃料管或固定到延伸管上，所述延伸管又固定到燃料管。 套管组件提供静电放电保护和防雷保护，因为隔离管保持与套管和燃料管的间隔距离，两者均由金属制成。 隔离管由电介质材料制成，但可以具有添加的导电颗粒以有助于消除静电电荷。 通过隔离管的电阻具有下限，以阻止感应雷电流通过组件的流动。 可以配置防雷等级。 可以通过使用热焊接，粘合剂或机械压力来固定套圈组件部件。
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公开(公告)号：US09061768B2
公开(公告)日：2015-06-23
申请号：US13277471
申请日：2011-10-20
CPC分类号： B64D37/00 , B64D37/005 , B64D37/32 , Y02T50/44 , Y10T29/4995
摘要： A mounting system for tubular structures within a wing structure provides for positioning of the tubular structure as it passes through wing ribs. The system provides for electrostatic protection from discharges between the rib and the tubular structure, and accommodates offset tubular positioning. A mounting flange is attached to an aperture in the wing rib, and the tubular structure is inserted through an aperture in the mounting flange. Once the tubular structure is positioned, a cushion mount comprising two pieces is inserted into the flange structure, holding the tubular structure in position in the mounting flange. The cushion mount may have a concentric aperture or an offset aperture to accommodate an offset positioned tubular structure in the wind rib aperture.
摘要翻译： 管状结构在翼结构内的安装系统提供了当管状结构穿过翼肋时的定位。 该系统提供静电防止肋与管状结构之间的排放，并适应偏移管状定位。 安装凸缘连接到翼肋中的孔，并且管状结构通过安装凸缘中的孔插入。 一旦管状结构被定位，将包括两个部件的缓冲垫安装在凸缘结构中，将管状结构保持在安装凸缘中的适当位置。 缓冲垫可以具有同心孔或偏移孔，以容纳风肋孔中的偏移定位的管状结构。
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公开(公告)号：US20130153046A1
公开(公告)日：2013-06-20
申请号：US13327850
申请日：2011-12-16
CPC分类号： F16L39/005 , B64D37/32 , B64D45/02 , F16L13/0245 , F16L13/103 , F16L25/01 , F16L25/025 , F16L25/03 , F16L47/03 , F16L47/24 , Y02T50/44 , Y10T137/0402
摘要： A fuel line assembly for an aircraft comprises a ferrule assembly comprising a ferrule affixed to an isolation tube, which may be directly affixed to a fuel tube or affixed to an extension tube, which in turn, is affixed to the fuel tube. The ferrule assembly provides electrostatic discharge protection and lightning protection as the isolation tube maintains a separation distance from the ferrule and fuel tube, both of which are made from metal. The isolation tube is made from a dielectric material, but which may have conductive particles added to aid in the dissipation of an electrostatic charge. The electrical resistance through the isolation tube has a lower limit to arrest the flow of the induced lightning current through the assembly. The amount of lightning protection afforded can be configured. The ferrule assembly components may be affixed by using thermo-welding, adhesive, or mechanical pressure.
摘要翻译： 用于飞行器的燃料管线组件包括套圈组件，其包括固定到隔离管的套圈，所述套圈可以直接固定到燃料管或固定到延伸管上，所述延伸管又固定到燃料管。 套管组件提供静电放电保护和防雷保护，因为隔离管保持与套管和燃料管的间隔距离，两者均由金属制成。 隔离管由电介质材料制成，但可以具有添加的导电颗粒以有助于消除静电电荷。 通过隔离管的电阻具有下限，以阻止感应雷电流通过组件的流动。 可以配置防雷等级。 可以通过使用热焊接，粘合剂或机械压力来固定套圈组件部件。
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公开(公告)号：US20130099067A1
公开(公告)日：2013-04-25
申请号：US13277471
申请日：2011-10-20
CPC分类号： B64D37/00 , B64D37/005 , B64D37/32 , Y02T50/44 , Y10T29/4995
摘要： A mounting system for tubular structures within a wing structure provides for positioning of the tubular structure as it passes through wing ribs. The system provides for electrostatic protection from discharges between the rib and the tubular structure, and accommodates offset tubular positioning. A mounting flange is attached to an aperture in the wing rib, and the tubular structure is inserted through an aperture in the mounting flange. Once the tubular structure is positioned, a cushion mount comprising two pieces is inserted into the flange structure, holding the tubular structure in position in the mounting flange. The cushion mount may have a concentric aperture or an offset aperture to accommodate an offset positioned tubular structure in the wind rib aperture.
摘要翻译： 管状结构在翼结构内的安装系统提供了当管状结构穿过翼肋时的定位。 该系统提供静电防止肋与管状结构之间的排放，并适应偏移管状定位。 安装凸缘连接到翼肋中的孔，并且管状结构通过安装凸缘中的孔插入。 一旦管状结构被定位，将包括两个部件的缓冲垫安装在凸缘结构中，将管状结构保持在安装凸缘中的适当位置。 缓冲垫可以具有同心孔或偏移孔，以容纳风肋孔中的偏移定位的管状结构。
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