Composite tubes for a fluid transport system

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United States of America Patent

PATENT NO 10633111
APP PUB NO 20170291717A1
SERIAL NO

15633735

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Abstract

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A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. In one illustrative embodiment, an apparatus includes a transport member. The transport member is configured for use in the fluid transport system. The transport member includes a material configured to reduce voltages and currents, induced in response to an electromagnetic event, along the transport member.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANY100 NORTH RIVERSIDE PLAZA CHICAGO IL 60606

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Axtell, John Thomas Bellevue, US 4 18
Irwin, James Patrick Renton, US 4 18
Johnson, Benjamin A Lynnwood, US 39 879
Minteer, David William Lake Tapps, US 6 55

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