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Browse by: INVENTOR PATENT HOLDER PATENT NUMBER DATE
 
 
Inventor:
Murphy; Jane Ann
Address:
Franklin, OH
No. of patents:
16
Patents:












Patent Number Title Of Patent Date Issued
8147922 Composition and method for a thermal coating system April 3, 2012
A thermal coating includes a substrate, a first coating layer, and a second coating layer. The substrate is selected from the group consisting of superalloys and ceramic matrix composites. The first coating layer comprises an alumina powder, a silica binder, and at least one additive
8007246 Methods and apparatus for coating gas turbine engines August 30, 2011
A method of fabricating a component for a gas turbine engine is provided. The method includes applying a bond coat to at least a portion of the component, applying a dense vertically cracked (DVC) thermal barrier coating to at least a portion of the bond coat using a spray mechanism
7842335 Field repairable high temperature smooth wear coating November 30, 2010
A chemical composition and method for repairing a thermal barrier coating on a component designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The method repairs a thermal barrier coating on a component that has su
7754043 Method for applying an optical coating to a surface of an article July 13, 2010
An optical coating is applied to an article surface of an article by providing a deposition substrate other than the article surface, wherein the deposition substrate is made of a removable material. The optical coating is thereafter deposited onto the deposition substrate. The optic
7749570 Method for depositing a platinum-group-containing layer on a substrate July 6, 2010
A method for depositing a platinum-group-containing layer on a substrate includes furnishing the substrate, and preparing a water-base paint containing metallic platinum-group powder, water, and a binder. The method further includes spraying the water-base paint overlying the substra
7695582 Method of forming ceramic layer April 13, 2010
A method for forming a ceramic layer on the surface of a turbine component. This method comprises the following steps: (a) providing a turbine component having a surface; (b) providing at least one ceramic tape overlaying the component surface; and (c) manually pressing the at least
7601400 Liquid electrostatic coating composition comprising corrosion resistant metal particulates and m October 13, 2009
A composition comprising a liquid mixture having: a corrosion resistant metal particulate component comprising aluminum-containing metal particulates, wherein the aluminum-containing metal particulates have a phosphate and/or silica-containing insulating layer; a glass-forming binder
7588797 Field repairable high temperature smooth wear coating September 15, 2009
A chemical composition and method for repairing a thermal barrier coating on a component designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The method repairs a thermal barrier coating on a component that has su
7544396 Electrostatic coating composition comprising corrosion resistant metal particulates and method f June 9, 2009
A composition comprising a corrosion resistant metal particulate component comprising aluminum-containing metal particulates, wherein the aluminum-containing metal particulates have a phosphate and/or silica-containing insulating layer; and a glass-forming binder component. Also disc
7473331 Method of applying an optical coating to an article surface January 6, 2009
An optical coating is applied to an article surface of an article by applying a first release system to a deposition substrate, and depositing the optical coating onto the deposition substrate. A second release system and transfer substrate is applied to the second face of the optica
7368164 Smooth outer coating for combustor components and coating method therefor May 6, 2008
A coating and method for overcoating a TBC on a component used in a high-temperature environment, such as the combustor section of an industrial gas turbine. The coating defines the outermost surface of the component and is formed of at least two layers having different compositions.
7250192 Sprayable noble metal coating for high temperature use directly on aircraft engine alloys July 31, 2007
A method of applying a heat-rejection coating directly on a substrate of a metallic component is disclosed. The steps include supplying a metallic component, such as of a gas turbine engine, before applying a reflective-coating mixture onto the component, wherein the reflective-coati
7093993 Apparatus and methods for cleaning and priming of coated surfaces August 22, 2006
Apparatus and methods for cleaning and repairing a thermal barrier coating on a component designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The apparatus is a handheld tool that includes an applicator and a flu
7090894 Bondcoat for the application of TBC's and wear coatings to oxide ceramic matrix August 15, 2006
A bond coat composition is provided for applying to the surface of a ceramic composite component between the composite substrate and the thermal barrier coat. The composition includes an alumina powder, a silica-yielding liquid, glass frits, and sufficient solvent to permit mixing of
6827969 Field repairable high temperature smooth wear coating December 7, 2004
A chemical composition and method for repairing a thermal barrier coating on a component designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The method repairs a thermal barrier coating on a component that has su
6720034 Method of applying a metallic heat rejection coating onto a gas turbine engine component April 13, 2004
A heat-rejection coating is applied to a metallic component of a gas turbine engine, preferably made of a nickel-base superalloy. A component surface is preferably pre-treated, as by polishing the component surface, thereafter pre-oxidizing the component surface, and thereafter applying










 
 
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