Georgia Tech Research Corporation

Airbus Operations (s.a.s.)

Onera (office National D'etudes Et De Recherches Aerospatiales)

Jason Hayes Nadler

Brent Karl Wagner

Pierre J Josso

William Judson Ready

Marie-Pierre Bacos

Florin Paun

Maud Lavieille

Robert L Rosson

Zhitao Kang

Bernd Kahn

Michael Beckert

Meredith Brooke Barta

Stéphane Gasser

Stephan Turano

Metal substrates comprising a colored coating and/or a protective coating disposed on at least a surface of the substrate. The colored coating can include a metal oxide coating integrally bonded to the terminal and produced by heat tinting or a titanium nitride containing material. The protective coating is derived from a material comprising one or more of aluminum oxide, silicon oxide, a superhydrophobic material, wherein the protective coating has a Scratch Resistance of at least about F, as determined by ASTM D336. Methods of making and using the coated metal substrates are also disclosed.

Methods to impart color and durable properties to substrates

A micro-channeled material is fabricated from a bundle of metal-plated polymer fibers by a process wherein the polymer fibers are heated to a first temperature and pyrolyzed in the presence of an inert gas at atmospheric pressure.

Method of producing a micro-channeled material at atmospheric pressure

Compositions and methods are described for transparent glass composite having nanoparticles therein that scintillate in the presence of nuclear radiation, particularly gamma rays, but also x-rays, alpha particles, beta particles, and neutrons. The transparent glass composites can be prepared by a melt/cool process to produce the transparent glass composite. The wavelength of light emitted by the transparent glass composite can be tailored based on the materials used to make the glass composite. A detector that utilizes the transparent glass composite can measure nuclear radiation from numerous sources.

Transparent glass scintillators, methods of making same and devices using same

A structural element used for attenuating aviation turbine noise is provided with pores () embodied in the form of cylindrical channels which are open on the first ends inside the turbine housing and closed on the opposite ends thereof, wherein the diameter (D) of each channel ranges approximately from 0.1 to 0.3 mm, each channel is remote at least along one part of the length thereof from the closest neighbors at a minimum distance ranging approximately from 0.02 to 0.3 mm and the ratio between the channel length and diameter thereof is of the order of 10.

Porous metal bodies used for attenuating aviation turbine noise

Growing community of inventors

Decatur, GA, United States of America

Jason Hayes Nadler