General Electric Company

Mark Rechtsteiner

Roy F Thornton

Mark Guenter Herwig

Bruce Edward Goodwin

Andrew Jay Skoog

Jane Ann Murphy

James Stephen Shaw

Matthew Bernard Buczek

William D Rouse

Electrostatic deposition of high performance powdered materials onto gas turbine surfaces. The process also includes post-deposition thermal staging of the deposited powder to provide a durable coating that will satisfy the demands of turbine engine operation. The process envisions application of organic-based powdered materials, glass/ceramic powdered materials and metal-based powdered materials and combinations thereof using electrostatic techniques to components exposed to low temperature operations, such as may be found in the front section of a gas turbine engine or to the exterior portions of an aircraft engine, and metal-containing glass ceramics, glass-ceramic materials, or materials that can be transformed into glass ceramic materials, when applied to components exposed to high temperature operations, such as may be found in the turbine and exhaust sections of a gas turbine engine or the flaps of an aircraft.

Electrostatic spray for coating aircraft engine components

A composition and method for cleaning gas turbine engines to remove fuel or lubricant residues. The composition can include a mixture of hydrofluorocarbon and hydrofluoroether. The method can include the step of directing a pressurized stream of the cleaning composition against one or more portions of the gas turbine engine to remove fuel and/or lubricant residues.

Composition for engine cleaning

Composition and method for engine cleaning

A nozzle includes a tube and a flared deflector extending coaxially from an outlet thereof. A stream of abrasive pliant shot is discharged through the nozzle and deflected radially outwardly from the deflector for abrading a shifting edge along an aperture in a workpiece surface.

Omnidirectional shot nozzle

Growing community of inventors

Cincinnati, OH, United States of America

Mark Rechtsteiner