General Nano LLC

Other

Composipole, Inc.

Thomas J Sorenson

Larry Allen Christy

Joseph E Sprengard

Chaminda Jayasinghe

B Jay Larson

A light-weight, highly-conductive material useful for repairing a lightning protection system in an aircraft. The material includes a nonwoven carbon fiber veil and a metal coating covering the veil. The veil includes a plurality of carbon fibers looped randomly throughout the veil and a binder material that binds the plurality of fibers together. The metal coating covers a portion of a surface of the plurality of bound fibers of the veil, and preferably the entire surface of both the plurality of bound fibers and the binder material, forming a highly-conductive network that follows the shape of the plurality of fibers in the veil. The areal weight is in a range from at least 5 grams per square meter (gsm), up to 12 gsm, and the sheet resistance is in a range from at least 0.5 ohms per square (Ω/□), up to 2Ω/□.

Light-weight, highly-conductive repair material

A heated composite tool, useful for forming, debulking, and/or curing prepreg materials, including a composite build structure having a shape of a composite part that is to be produced, configured to receive and support prepreg materials during lay-up, and including a heating structure physically coupled to the composite build structure, and comprising at least one heating element, including a carbon nanotube structured layer defining a current path having first and second ends and first and second electrical terminals electrically coupled to the first and second ends and a first isolation ply disposed between the composite build structure and the at least one heating element, the first isolation ply forming an electrical insulating gap between the at least one heating element and the composite build structure, wherein the carbon nanotube structured layer is responsive to an electromotive force applied across the first and second electrical terminals to heat the tool.

Heated composite tool and method for building and use

Disclosed embodiments include hollow composite utility pole, cross arm, and brace structures and methods of manufacture of the same using fire retardant materials. Poles, cross arm, and brace structures may be manufactured using a fire resistant resin impregnated, or resin wetted, filament roving that is wound onto a mandrel, pultruded or otherwise formed into a structural part. Various pole structures and manufacturing methods are described, including chemically bonded sleeve joint structures for poles of varying size.

Lightweight fire resistant composite utility pole, cross arm and brace structures

A positioning system is provided for positioning a chair-mounted table. The positioning system utilizes four major interconnected components which are capable of rotating around four different axes to position the table in a large variety of positions and orientations. The first axis is parallel to the ground, the second axis is substantially perpendicular to the first axis, the third axis is perpendicular to the second axis, and the fourth axis is substantially 45 degrees from the third axis. The table attached to the positioning system may be moved forward and backward relative to the user, it may be rotated to various angular positions, it may be swung forward to allow the user to sit down and get up, it may be placed on the side of the chair to make a side table, and it may be swung down to the side of the chair to occupy little space and allow the chair to be used with a stand-alone desk or table.

Growing community of inventors

Cottonwood Heights, UT, United States of America

Thomas J Sorenson