The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 20, 2015

Filed:

Jan. 23, 2013
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

David William Minteer, Lake Tapps, WA (US);

James Patrick Irwin, Renton, WA (US);

Benjamin A. Johnson, Lynnwood, WA (US);

John Thomas Axtell, Bellevue, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H05F 3/00 (2006.01); B64D 45/02 (2006.01); F16L 25/02 (2006.01); F17D 1/00 (2006.01); F16L 9/14 (2006.01); H05F 1/00 (2006.01); F16L 21/06 (2006.01); F16L 25/01 (2006.01);
U.S. Cl.
CPC ...
B64D 45/02 (2013.01); F16L 9/14 (2013.01); F16L 21/065 (2013.01); F16L 25/01 (2013.01); F16L 25/025 (2013.01); F16L 25/026 (2013.01); F17D 1/00 (2013.01); H05F 1/00 (2013.01); Y10T 137/8593 (2013.01);
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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