Fluid transport system for preventing electrical discharge

A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system (100) in an aerospace vehicle (106). The aerospace vehicle (106) is operated. The fluid transport system (100) in the aerospace vehicle (106) is comprised of materials selected suc...

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Bibliographische Detailangaben
Hauptverfasser:	JOHNSON, BENJAMIN A, MINTEER, DAVID WILLIAM, AXTELL, JOHN THOMAS, IRWIN, JAMES PATRICK
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING JOINTS OR FITTINGS FOR PIPES LIGHTING MEANS FOR THERMAL INSULATION IN GENERAL MECHANICAL ENGINEERING PIPES SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system (100) in an aerospace vehicle (106). The aerospace vehicle (106) is operated. The fluid transport system (100) in the aerospace vehicle (106) is comprised of materials selected such that the fluid transport system (100) has an electrical configuration. The intensity of the electrical discharge that occurs within the fluid transport system (100) during operation of the aerospace vehicle (106) is reduced to within selected tolerances by the electrical configuration of the fluid transport system (100). C%4 0)0 o / r.0 ~C.0 CNo L() 0'