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 protect
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.
대표청구항▼
1. A ferrule assembly comprising: a metallic ferrule comprising a cylindrical shape having a first end, a second end, an outside surface extending from the first end to the second end, and an inside surface opposite the outside surface and extending from the first end to the second end, wherein the
1. A ferrule assembly comprising: a metallic ferrule comprising a cylindrical shape having a first end, a second end, an outside surface extending from the first end to the second end, and an inside surface opposite the outside surface and extending from the first end to the second end, wherein the first end comprises a first lip and a second lip projecting outwards from the outside surface and forming a channel configured to receive an O-ring; andan isolation tube comprising a non-metallic material and comprising a first inner band and a first outer band, the first inner band and the first outer band forming a groove for receiving the second end of the metallic ferrule such that the first inner band encircles the inside surface of the second end of the metallic ferrule and the first outer band encircles the outside surface of the second end of the metallic ferrule to provide a concentric arrangement of the first outer band, the groove, and the first inner band around a central axis of the isolation tube, wherein the isolation tube is configured to receive a fuel tube and provide a separation distance between the fuel tube and the metallic ferrule. 2. The ferrule assembly of claim 1, wherein the metallic ferrule further comprises a body section comprising a plurality of holes on a side wall of the metallic ferrule. 3. The ferrule assembly of claim 2, wherein the isolation tube comprises PEEK or PEKK. 4. The ferrule assembly of claim 3, wherein the isolation tube comprising PEEK or PEKK (or any other suitable material) is rendered conductive by adding conductive filler to provide electrostatic conductivity. 5. The ferrule assembly of claim 4, wherein the conductive filler is used to control electrical resistance so as to fall within a permissible range through the isolation tube from the metallic ferrule to the fuel tube. 6. The ferrule assembly of claim 5, wherein the permissible range of the electrical resistance through the isolation tube does not exceed an upper limit of 100 mega-ohms. 7. The ferrule assembly of claim 5, wherein the lower limit of the permissible range of the electrical resistance through the isolation tube is not less than 8,000 ohms at 400 volts when the separation distance is at least 0.2 inches. 8. The ferrule assembly of claim 5, wherein the lower limit of the permissible range of the electrical resistance through the isolation tube is not less than 100,000 ohms at 5,000 volts when the separation distance is at least 3 inches. 9. The ferrule assembly of claim 3, wherein the isolation tube is rendered conductive by adding conductive filler to provide electrostatic conductivity, wherein the electrostatic conductivity is used to control an electrical resistance to fall within a permissible range through the isolation tube from the metallic ferrule to the fuel tube. 10. The ferrule assembly of claim 2, wherein the holes on the side wall of the metallic ferrule are filled by a material of the isolation tube forming a mechanical lock. 11. The ferrule assembly of claim 1, wherein the isolation tube further comprises an aluminum extension tube affixed to the isolation tube using an adhesive and is configured to provide the separation distance between the extension tube and the metallic ferrule. 12. The ferrule assembly of claim 11, wherein the extension tube is affixed to the isolation tube by one of adhesion using an adhesive, thermo-welding, or spin welding. 13. The ferrule assembly of claim 11, wherein the isolation tube comprises a second inner band and a second outer band, wherein the second inner band and the second outer band from a second groove configured to receive the extension tube. 14. The ferrule assembly of claim 1, wherein the fuel tube comprises a metal and further comprises a body section comprising a plurality of holes on a side wall of the fuel tube. 15. The ferrule assembly of claim 14, wherein the holes in the fuel tube are filled by material of the isolation tube forming a mechanical lock. 16. The ferrule assembly of claim 1, wherein the metallic ferrule is affixed to the isolation tube by one of an adhesion using an adhesive, thermo-welding, or spin welding. 17. The ferrule assembly of claim 1, wherein the isolation tube comprises a second inner band and a second outer band, wherein the second inner band and the second outer band form a second groove configured to receive the fuel tube. 18. The ferrule assembly of claim 1, wherein the extension tube comprises a metal and further comprises a body section comprising a plurality of holes on a side wall of the extension tube. 19. The ferrule assembly of claim 1, wherein the separation distance is at least 0.2 inches and is configured to withstand a flashover through air from the metallic ferrule to the fuel tube at 400 volts at 40,000 feet of altitude. 20. The ferrule assembly of claim 1, wherein the separation distance is at least 3 inches and is configured to withstand a flashover through air from the metallic ferrule to the fuel tube at 5,000 volts at 40,000 feet of altitude.
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이 특허에 인용된 특허 (11)
West, Colin John; Sutton, David Alistair, Aircraft joint and bonding lead.
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