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公开(公告)号：US20160123512A1
公开(公告)日：2016-05-05
申请号：US14992494
申请日：2016-01-11
申请人： The Boeing Company
IPC分类号： F16L39/00
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：US20130327888A1
公开(公告)日：2013-12-12
申请号：US13747732
申请日：2013-01-23
申请人： THE BOEING COMPANY
发明人： Kevin O'Brien Gaw , Nathan Michael Kelley , John Thomas Axtell , James Patrick Irwin , David William Minteer , Diego A. Velasco
CPC分类号： B64D45/02 , B60R16/06 , B63B43/00 , F16L9/14 , F16L21/065 , F16L25/01 , F16L25/025 , F16L25/026 , F17D1/00 , F17D5/08 , H05F1/00 , Y10T137/8593
摘要： A method and apparatus for conducting an electrical current between a first transport member and a second transport member. In one illustrative embodiment, a coupling assembly comprises a first fitting associated with a first end of a first transport member, a second fitting associated with a second end of a second transport member, and a seal. The seal is configured for placement around the first fitting and the second fitting when the first end of the first transport member is positioned relative to the second end of the second transport member. The seal is further configured to seal an interface between the first transport member and the second transport member. The seal is comprised of a material configured such that the seal has a level of conductivity within a selected range and such that a conductive pathway is formed between the first transport member and the second transport member.
摘要翻译： 一种用于在第一输送构件和第二输送构件之间进行电流的方法和装置。 在一个说明性实施例中，联接组件包括与第一输送构件的第一端相关联的第一配件，与第二输送构件的第二端相关联的第二配件和密封件。 当第一输送构件的第一端相对于第二输送构件的第二端定位时，密封件构造成围绕第一配件和第二配件放置。 密封件进一步构造成密封第一输送构件和第二输送构件之间的界面。 密封件由构造成使得密封件具有在所选范围内的导电率水平并且使得在第一输送构件和第二输送构件之间形成导电通路的材料构成。
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公开(公告)号：US09169029B2
公开(公告)日：2015-10-27
申请号：US13747732
申请日：2013-01-23
申请人： The Boeing Company
发明人： Kevin O'Brien Gaw , Nathan Michael Kelley , John Thomas Axtell , James Patrick Irwin , David William Minteer , Diego A. Velasco
CPC分类号： B64D45/02 , B60R16/06 , B63B43/00 , F16L9/14 , F16L21/065 , F16L25/01 , F16L25/025 , F16L25/026 , F17D1/00 , F17D5/08 , H05F1/00 , Y10T137/8593
摘要： A method and apparatus for conducting an electrical current between a first transport member and a second transport member. In one illustrative embodiment, a coupling assembly comprises a first fitting associated with a first end of a first transport member, a second fitting associated with a second end of a second transport member, and a seal. The seal is configured for placement around the first fitting and the second fitting when the first end of the first transport member is positioned relative to the second end of the second transport member. The seal is further configured to seal an interface between the first transport member and the second transport member. The seal is comprised of a material configured such that the seal has a level of conductivity within a selected range and such that a conductive pathway is formed between the first transport member and the second transport member.
摘要翻译： 一种用于在第一输送构件和第二输送构件之间进行电流的方法和装置。 在一个说明性实施例中，联接组件包括与第一输送构件的第一端相关联的第一配件，与第二输送构件的第二端相关联的第二配件和密封件。 当第一输送构件的第一端相对于第二输送构件的第二端定位时，密封件构造成围绕第一配件和第二配件放置。 密封件进一步构造成密封第一输送构件和第二输送构件之间的界面。 密封件由构造成使得密封件具有在所选范围内的导电率水平并且使得在第一输送构件和第二输送构件之间形成导电通路的材料构成。
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公开(公告)号：US09746117B2
公开(公告)日：2017-08-29
申请号：US14992494
申请日：2016-01-11
申请人： The Boeing Company
IPC分类号： F16L39/00 , B64D37/32 , F16L13/02 , F16L13/10 , F16L25/01 , F16L25/02 , F16L25/03 , F16L47/03 , F16L47/24 , B64D45/02
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.
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