Honeywell International Inc.

Jeffrey P Armstrong

Dave Narasimhan

Thomas E Strangman

Keith R Karasek

A method for forming a carbon deposit inhibiting thermal barrier coating for an internal element or component of a gas turbine engine. Such coating includes a layer of thermal barrier material coated onto the surface of an engine component that will be exposed to the flow of burning engine gases. Such coating further includes a layer of carbon deposit inhibiting material coated on top of the layer of thermal barrier material.

Method for forming a carbon deposit inhibiting thermal barrier coating for combustors

A carbon deposit inhibiting thermal barrier coating for an internal element or component in a gas turbine engine. Such coating includes a layer of thermal barrier material coated onto the surface of an engine component that will be exposed to the flow of burning engine gases. Such coating further includes a layer of carbon deposit inhibiting material coated on top of the layer of thermal barrier material.

Growing community of inventors

Tempe, AZ, United States of America

Jeffrey P Armstrong