Fluid transport system for preventing electrical discharge
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United States of America Patent
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Oct 20, 2015
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N/A
app pub date -
Jan 23, 2013
filing date -
Jun 8, 2012
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Abstract
A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. The aerospace vehicle is operated. The fluid transport system in the aerospace vehicle is comprised of materials selected such that the fluid transport system has an electrical configuration. The intensity of the electrical discharge that occurs within the fluid transport system during operation of the aerospace vehicle is reduced to within selected tolerances by the electrical configuration of the fluid transport system.
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