General Electric Company

Ann Melinda Ritter

Melvin Robert Jackson

Bernard Patrick Bewlay

Paul Leonard Dupree

Ronald Scott Bunker

Lawrence Bernard Kool

Donald N Wemple, Jr

Curtis Alan Johnson

Ji-Cheng Zhao

John R Hughes

Don Mark Lipkin

Nesim Abuaf

Raul Basilio Rebak

Paul A Siemers

Yuk-Chiu Lau

Michael Francis Xavier Gigliotti

Michael F Gigliotti, Jr

Charles Gitahi Mukira

Raymond Alan White

Laurent Cretegny

John Brian McDermott

Aaron Todd Frost

Robert Patrick Campbell

Renee Bushey Rohling

Paul Vincent Crimi

Ching-Pang Lee

Jerome Johnson Tiemann

Bin Wei

James Anthony Ruud

John Eric Tkaczyk

Canan Uslu Hardwicke

Stephen Francis Rutkowski

Pazhayannur Ramanathan Subramanian

Dennis Michael Gray

Stephen Joseph Ferrigno

Constantinos Minas

Craig Douglas Young

Scott Andrew Weaver

Judson Sloan Marte

Liang Jiang

Adrian M Beltran

Francisco J Cunha

David Robert Schumacher

Roger John Petterson

Sanjay M Correa

Mark Dean Pezzutti

Wayne Alan Demo

Donald R Spriggs

Mitchell R Cohen

Francis Lawrence Kirkpatrick

Stewart William Beitz

Myron Clyde Muth

Lance Gordon Peterson

Ross Anthony McLean

Jeffrey Alan Graves

Donald Norman Wemple, Jr

John Brian Mcdermott

Magdi N Azer

The present disclosure is directed to the use and manufacture of cooling features within a component used in a hot gas path, such as within a turbine. In one embodiment, channels are formed within an external surface of the component and filled with a removable material. The external surface and channels may then be coated with one or more layers, such as a structural layer and/or top coat. The removable material may then be removed to leave the channels free of the removable material.

Turbine components with cooling features and methods of manufacturing the same

Methods of fabricating coated components using multiple types of fillers are provided. One method comprises forming one or more grooves in an outer surface of a substrate. Each groove has a base and extends at least partially along the outer surface of the substrate. The method further includes disposing a sacrificial filler within the groove(s), disposing a permanent filler over the sacrificial filler, disposing a coating over at least a portion of the substrate and over the permanent filler, and removing the first sacrificial filler from the groove(s), to define one or more channels for cooling the component. A component with a permanent filler is also provided.

Component and methods of fabricating a coated component using multiple types of fillers

Methods of fabricating coated components using multiple types of fillers are provided. One method comprises forming one or more grooves in an outer surface of a substrate. Each groove has a base and extends at least partially along the outer surface. A sacrificial filler is deposited within the groove, a second filler is deposited over the sacrificial filler, and a coating is disposed over at least a portion of the outer surface and over the second filler. The method further includes removing the sacrificial filler and at least partially removing the second filler from the groove(s), to define one or more channels for cooling the component.

Methods of fabricating a coated component using multiple types of fillers

The present invention provides a method for forming a refractory metal-intermetallic composite. The method includes providing a first powder comprising a refractory metal suitable for forming a metal phase; providing a second powder comprising a silicide precursor suitable for forming an intermetallic phase; blending the first powder and the second powder to form a powder blend; consolidating and mechanically deforming the powder blend at a first temperature; and reacting the powder blend at a second temperature to form the metal phase and the intermetallic phase of the refractory metal-intermetallic composite, wherein the second temperature is higher than the first temperature.

High-temperature composite articles and associated methods of manufacture

A method for evaluating the thermal exposure of a selected metal component which has been exposed to changing temperature conditions is described. The voltage distribution on a surface of the metal component, or on a metallic layer which lies over the component, is first obtained. The voltage distribution usually results from a compositional change in the metal component. The voltage distribution is then compared to a thermal exposure-voltage model which expresses voltage distribution as a function of exposure time and exposure temperature for a reference standard corresponding to the metal component. In this manner, the thermal exposure of the selected component can be obtained. A related device for evaluating the thermal exposure of a selected metal component is also described.

Methods and devices for evaluating the thermal exposure of a metal article

A shell mold for casting molten material to form an article is described. The mold includes a shell for containing the molten material, formed from at least one of yttrium silicates, zirconium silicates, hafnium silicates, and rare earth silicates. The mold also includes a facecoat disposed on an inner surface of the shell that contacts the molten material. The facecoat can be made from the materials described above. A method of casting a niobium-silicide article is also described, using the shell mold described herein. A method of making the ceramic shell mold is described as well, along with a slurry composition used in the manufacture of the shell mold.

Shell mold for casting niobium-silicide alloys, and related compositions and processes

A method for removing an oxide material from a crack in a substrate, the method includes: applying a slurry paste comprising a fluoride salt to the crack; heating the slurry paste and the crack to at least a melting point of the fluoride salt to form a reaction product; and removing the reaction product.

Method for removing oxide from cracks in turbine components

A on-line method is provided for detecting wear and/or damage to gas turbine parts. Preferred embodiments of the invention provide a gas turbine comprising parts with smart coatings and collection and detection means to measure wear and erosion of gas turbine parts. In other preferred embodiments, smart coatings are provided comprising chemical taggants that can be collected and detected downstream, thus providing an on-line or in situ evaluation technology for wear and damage to gas turbine parts.

Smart coating system with chemical taggants for coating condition assessment

A roughened bond coat comprises a screen that includes interwoven wires defining openings and a metallic material disposed on the screen. The screen and metallic material form a roughened bond coat possessing an uneven, undulated, and irregular surface. The metallic material may be one of a slurry and a powder, and applied by coating and spraying, respectively. A thermal barrier coating system, which is formed with and incorporates the roughened bond coat, exhibits greater adhesion of a thermal barrier coating and bond coat due to an increased interfacial surface area provided by the uneven, undulated, and irregular surface.

Roughened bond coats for a thermal barrier coating system and method for producing

A composition comprises cobalt; chromium; carbon; boron; zirconium; aluminum; at least one refractory material; and nickel. The composition is used as a repair material for repairing superalloy articles in a repair process.

Repair material, process of repairing using the repair material, and article repaired

A bond coat and method of forming a bond coat for a thermal barrier coating system are set forth. The bond coat is a roughened bond coat and comprises a layer possessing an uneven, undulated, and irregular surface. The layer is formed of a metal powder mixture disposed on a substrate, such as a turbine component, by high velocity oxygen fuel spraying. The metal powder mixture comprises at least one of a first powder having a first melting point and a second powder having a second melting point that is higher than the first melting point. The bond coat's uneven, undulated, and irregular surface enhances prevention of de-bonding of elements in a thermal barrier coating system.

Roughened bond coat for a thermal barrier coating system and method for producing

A method of providing a roughened bond coat, for example in a thermal barrier coating system, comprises providing an oxidation-resistant plasma-sprayed layer onto a substrate and disposing a slurry overlayer on the oxidation-resistant plasma-sprayed layer. These steps form a roughened bond coat possessing an uneven, undulated, and irregular surface. A roughened bond coat in a thermal barrier coating system reduces de-bonding of the bond coat and a thermal barrier coating layer, which is desirable to maintain the insulation features of the thermal barrier coating system.

Roughened bond coat and method for producing using a slurry

A continuously-graded bond coat comprises a gradient of at least one material characteristic value. The gradient extends from a first material characteristic value at a first surface region to a second material characteristic value at a second surface region. The continuously-graded bond coat can be used in a thermal barrier coating system. A source ingot for forming the continuously-graded bond coat comprises aluminum, in an atomic percent range from about 50.0 to less than about 100.0; chromium in an atomic percent range from about 5.0 to about 40.0; silicon in an atomic percent range from about 1.0 to about 17.0; zirconium in an atomic percent range from about a trace to about a 0.5, yttrium in an atomic percent range from a trace to about 2.0; and hafnium in an atomic percent range from about 0.5 to about 2.0. A method for forming the continuously-graded bond coat with the gradient is also provided by the invention.

Continuously-graded bond coat and method of manufacture

Method for producing a roughened bond coat using a slurry

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Niskayuna, NY, United States of America

Ann Melinda Ritter