Method of installing fuel lines in an aircraft

Patent metadata

Field	Value
Publication number	US-9746117-B2
Application number	US-201614992494-A
Country	US
Kind code	B2
Filing date	Jan 11, 2016
Priority date	Dec 16, 2011
Publication date	Aug 29, 2017
Grant date	Aug 29, 2017

Abstract

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.

First claim

The invention claimed is:

1. A method of installing fuel lines in an aircraft comprising the operations of:
affixing an isolation tube at a first end to a first fuel tube directly or via an extension tube in a manner that prevents relative movement between the isolation tube and the first fuel tube;
affixing a ferrule to a second end of the isolation tube in a manner that prevents relative movement between the isolation tube and the ferrule, wherein the second end of the isolation tube comprises a second end inner band and a second end outer band defining a second end groove, and wherein affixing the ferrule to the second end of the isolation tube comprises inserting a portion of the ferrule into the second end groove;
installing the first fuel tube in a structure of the aircraft; and
affixing the ferrule to a fuel system component, wherein any of the first three operations can be performed in any order.

2. The method of claim 1 , wherein affixing the ferrule to the fuel system component comprises affixing the ferrule to a coupler.

3. The method of claim 2 , wherein affixing the ferrule to the isolation tube comprises either:
thermo-welding or spin welding the ferrule to the isolation tube, or
using an adhesive to affix the ferrule to the isolation tube.

4. The method of claim 1 , wherein the first end of the isolation tube comprises a first end inner band and a first end outer band defining a first end groove, and wherein affixing the first end of the isolation tube to the first fuel tube comprises inserting a portion of the first fuel tube into the first end groove.

5. A method of installing fuel lines in an aircraft comprising the operations of:
affixing an isolation tube at a first end to a first fuel tube directly or via an extension tube in a manner that prevents relative movement between the isolation tube and the first fuel tube, wherein the first end of the isolation tube comprises a first end inner band and a first end outer band defining a first end groove, and wherein affixing the first end of the isolation tube to the first fuel tube comprises inserting a portion of the first fuel tube into the first end groove;
affixing a ferrule to a second end of the isolation tube in a manner that prevents relative movement between the isolation tube and the ferrule;
installing the first fuel tube in a structure of the aircraft; and
affixing the ferrule to a fuel system component, wherein any of the first three operations can be performed in any order.

6. The method of claim 5 , wherein affixing the ferrule to the fuel system component comprises affixing the ferrule to a coupler.

7. The method of claim 6 , wherein affixing the ferrule to the isolation tube comprises either:
thermo-welding or spin welding the ferrule to the isolation tube, or
using an adhesive to affix the ferrule to the isolation tube.

Assignees

• Boeing Co

Inventors

• Hansom Christopher Michael
• Irwin James P
• Kelley Nathan Michael

Classifications

• B64D45/02

  Lightning protectors; Static dischargers · CPC title

• F16L25/03

  in non-disconnectable pipe joints · CPC title

• F16L13/103

  Adhesive joints · CPC title

• Y02T50/44

  Cross-Sectional Technologies · mapped topic

• B64D37/32 Primary

  Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title