Title:
COMPOSITE TUBE FOR FLUID TRANSPORT SYSTEM
Document Type and Number:
Japanese Patent JP2018112318
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a method and an apparatus for limiting flow of an electric current, induced by an event such as lightning or an electrical fault, along a fluid transport system and allowing electrostatic dissipation along the fluid transport system.SOLUTION: A method and an apparatus are for reducing intensity of electrical discharge that occurs within a fluid transport system in aerospace transport means. In one embodiment, the apparatus comprises a transport member. The transport member is configured for use in the fluid transport system. The transport member consists of a material configured to reduce a voltage and a current, induced in response to an electric event, along the transport member.SELECTED DRAWING: Figure 1
Inventors:
KEVIN O'BRIEN GAW
NATHAN MICHAEL KELLEY
JOHN THOMAS AXTELL
JAMES PATRICK IRWIN
DAVID WILLIAM MINTEER
DIEGO A VELASCO
BENJAMIN A JOHNSON
NATHAN MICHAEL KELLEY
JOHN THOMAS AXTELL
JAMES PATRICK IRWIN
DAVID WILLIAM MINTEER
DIEGO A VELASCO
BENJAMIN A JOHNSON
Application Number:
JP2018053923A
Publication Date:
July 19, 2018
Filing Date:
March 22, 2018
Export Citation:
Assignee:
BOEING CO
International Classes:
F16L25/01; B64D37/32; F16L9/00; F16L23/06; H05F3/02
Domestic Patent References:
| JP2010126133A | 2010-06-10 | |||
| JP2007500827A | 2007-01-18 |
Foreign References:
| US20120056416A1 | 2012-03-08 | |||
| WO2012032406A2 | 2012-03-15 | |||
| US20100122749A1 | 2010-05-20 |
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation