ELECTRICITY CONDUCTIVE MATERIAL

Japanese Patent JP2018052798

A

PROBLEM TO BE SOLVED: To provide conductive material improved compared with the previous ones as a protection film for accumulated electric charge applied to a surface of a moving transporter, which responds to demand that a surface coating for an airplane needs to diffuse accumulated electric charge through an electricity conductive material, and have corrosion durability to rain, ultraviolet light tolerance, high temperature and low temperature tolerance, flexibility, tolerance to damage caused by sand, and hail as well as compatibility with other chemicals which are added to improve its physical properties, and affinity with an underlayer.SOLUTION: A carbon allotrope material produced by applying a first material comprising polymer and sulfonic acid to a carbon allotrope material of a sheet material comprising carbon nano-tube, graphene, fullerene, or mixture thereof to form a second material, and curing the second material.EFFECT: To provide a protection film improved compared with the previous ones, which is obtained by applying said conductive carbon allotrope material to a surface of a substrate, including a part of a transporter.SELECTED DRAWING: None

PATRICK J KINLEN
DANIEL A CHARLES

JP2017159295A

April 05, 2018

August 22, 2017

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BOEING CO

C01B32/158; B64C1/00; B64D45/02; C01B32/168; C08K3/04; C08K7/06; C08L25/04; C08L29/14; C08L33/08; C08L63/00; C08L65/00; C08L67/00; C08L71/00; C08L75/04; C08L79/02; C08L81/04; C08L101/12; H01B1/00; H01B1/04; H01B1/12; H01B1/22; H01B13/00

JP2011124029A	2011-06-23
JP2014503387A	2014-02-13
JP2007534780A	2007-11-29
JP2012526724A	2012-11-01

WO2016126827A1

2016-08-11

Minoru Yoshida
Tatsuya Tanaka
Yasumitsu Suzuki
Nao Usui
Fumiaki Doi
Keita Kobuchi
Shintaro Suzuki

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