General Electric Company

Baker Hughes Oilfield Operations LLC

Vetco Gray Inc.

Global Nuclear Fuel - Americas, LLC

Dennis Michael Gray

Marcus P Borom

Curtis Alan Johnson

Yuk-Chiu Lau

Warren Arthur Nelson

Ronald Scott Bunker

Don Mark Lipkin

Pazhayannur Ramanathan Subramanian

Krishnamurthy Anand

Todd Charles Curtis

Wayne Charles Hasz

Carey Shawn Rogers

Young Jin Kim

Dalong Zhong

Melvin Robert Jackson

Bin Wei

Lawrence Bernard Kool

Farshad Ghasripoor

Gregory Alan Steinlage

Thomas Robert Raber

Surinder Singh Pabla

Michael Scott Hebert

Leonardo Ajdelsztajn

Anthony Mark Thompson

Steven Alfred Tysoe

David W White

Richard Arthur Nardi, Jr

Yang-Pi Lin

Thomas C Tiearney

Srinidhi Sampath

Timothy Francis Bethel

Olav Rommetveit

Hans Aunemo

Alain Demers

Charles Beaty Patterson

Jon Conrad Schaeffer

Christopher Edward Wolfe

James Anthony Ruud

Kripa K Varanasi

Lawrence E Szala

Ann Melinda Ritter

Scott Andrew Weaver

Raymond Alan White

Peter Louis Andresen

Sundeep Kumar

Tao Deng

Iacopo Giovannetti

Massimo Giannozzi

Margaret Louise Blohm

John R Rairden, Iii

Robert Anthony Fusaro, Jr

Nitin Bhate

Lee E Rumaner

Padmaja Parakala

Michael John Danyluk

Richard L Mehan

Raul Basilio Rebak

Eugenio Giorni

Nuo Sheng

John Peter Fura

Luc Stephane Leblanc

Anand Krishnamurthy

Liangheng Qiu

Chek Beng Ng

Kivilcim Onal

Lyon Euiyeol Hong

Paul Matthew Thomas

Ming Feng Hsu

Russell L McCarron

Nicole Barbara Piche

Krishnamurhty Anand

John Francis Van Nest

David William White

Francesco Sorbo

Carlo Del Vescovo

Fabio D'introno

Fabio D'INTRONO

A centrifugal pump component for an oil and gas well pump includes a substrate with an outer surface configured to contact oil and gas well fluid. The component further includes a coating formed on at least a portion of the outer surface. The coating includes a combination of hard particles and a metal matrix.

Oil and gas well pump components and method of coating such components

A system for use in coating an interior surface of an object is provided. The system includes a vacuum chamber enclosure defining an interior configured to receive the object, and a cathode coupled to the vacuum chamber enclosure. The cathode is fabricated from a coating material and has an outer surface. The cathode is configured such that when a current is applied to the cathode, an arc is formed on the outer surface and the coating material is removed from the cathode to form a cloud of coating material. The system also includes a collimator configured to be positioned between the cathode and the object configured to focus the cloud into a beam of coating material and to direct the beam towards the object, and a magnet configured to alter a path of the beam such that the beam is directed towards the interior surface of the object.

Systems and method of coating an interior surface of an object

There is provided a fuel rod assembly comprising a first component of a zirconium-based material. The first component is in contact with or is located adjacent to a second component of a material different from the zirconium-based material, e.g. a nickel-based or iron-based alloy. A coating is disposed on an outer surface of the first component, which is effective to reduce an electrochemical corrosion potential difference between the first component and the second component relative to an electrochemical corrosion potential difference between the first component and the second component without the coating.

Fuel rod assembly and method for mitigating the radiation-enhanced corrosion of a zirconium-based component

One aspect of the present invention includes an article. The article includes a substrate and a coating disposed on the substrate, wherein the coating includes a plurality of cermet particles bonded along their prior particle boundaries. The plurality of cermet particles have a median particle size less than about 5 microns and less than 25 percent of the plurality of cermet particles include melted and re-solidified particles. Gate valves are also presented.

Coating methods and coated articles

A seal system, for an apparatus that includes a rotatable portion with airfoils coupled thereto and a stationary portion with an inner surface, includes an abradable portion including at least one abradable layer of an abradable material formed over the inner surface. The seal system also includes an abrading portion disposed over at least a portion of a substrate of the airfoil. The abrading portion includes at least one abrading layer formed on at least a portion of the substrate and a plurality of abrasive particles embedded within the abrading layer. The plurality of abrasive particles includes at least one of substantially all of one of tantalum carbide (TaC), aluminum oxide (AlO), and ziconia (ZrO), cubic boron nitride (cBN) and AlOin predetermined ratios, cBN, AlOand ZrOin predetermined ratios, AlOand ZrOfused together in predetermined ratios, and TaC and AlOin predetermined ratios.

Seal systems for use in turbomachines and methods of fabricating the same

A composite composition that includes an MCrAlX alloy and a nano-oxide ceramic is disclosed. In the formula, M includes nickel, cobalt, iron, or a combination thereof, and X includes yttrium, hafnium, or a combination thereof, from about 0.001 percent to about 2 percent by weight of the alloy. The amount of the nano-oxide ceramic is greater than about 40 percent, by volume of the composition. A protective covering that includes the composite composition is also disclosed. The protective covering can be attached to a tip portion of a blade with a braze material. A method for joining a protective covering to a tip portion of a blade, and a method for repair of a blade, are also provided.

Composite composition for turbine blade tips, related articles, and methods

A method of fabricating a component is provided. The component includes a substrate that has at least one interior space. The method includes forming one or more grooves in the component. Each groove extends at least partially along an outer surface of the substrate and narrows at an opening thereof, such that each groove is re-entrant shaped. A cross-sectional area A of each groove is in a range of about 2 to about 3 times an area R=W*D, where W is the width of the opening and D is the depth of the re-entrant-shaped groove. Components with grooves formed in the substrate and components with grooves formed at least partially in a structural coating are also provided.

Components with re-entrant shaped cooling channels and methods of manufacture

A component is disclosed. The component comprises a substrate comprising an outer surface and an inner surface, where the inner surface defines at least one hollow, interior space, where the outer surface defines one or more grooves, and where each of the one or more grooves extends at least partially along the surface of the substrate and has a base. One or more access holes extend through the base of a respective groove to place the groove in fluid communication with respective ones of the at least one hollow interior space. The component further comprises a coating disposed over at least a portion of the substrate surface, where the coating comprises one or more layers. At least one of the layers defines one or more permeable slots, such that the respective layer does not completely bridge each of the one or more grooves. The grooves and the coating together define one or more channels for cooling the component.

Component and methods of fabricating and coating a component

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

A gate valve has a body, the body having a cavity and a flow passage intersecting the cavity. A seat is mounted to the body at the intersection of the flow passage and the cavity. A gate is installed at the cavity and has an engaging face that slidingly engages the seat while the gate is being moved between open and closed positions. The end faces between a seat pocket and the seat are hard-coated and smooth-finished to provide sealing when mated. The hardcoated pocket and seat sealing surfaces extend the life of the valve by eliminating the need for an elastomeric seal of limited life.

Gate valve seat and seat ring

A component is disclosed. The component comprises a substrate comprising an outer surface and an inner surface, where the inner surface defines at least one hollow, interior space, where the outer surface defines one or more grooves, and where each of the one or more grooves extends at least partially along the surface of the substrate and has a base. One or more access holes extend through the base of a respective groove to place the groove in fluid communication with respective ones of the at least one hollow interior space. The component further comprises a coating disposed over at least a portion of the substrate surface, where the coating comprises one or more layers. At least one of the layers defines one or more permeable slots, such that the respective layer does not completely bridge each of the one or more grooves. The grooves and the coating together define one or more channels for cooling the component. Methods for fabricating and coating a component are also provided.

Methods of fabricating and coating a component

The present invention provides methods for manufacturing an article having a wetting-resistant surface. The method includes providing a mixture comprising a plurality of micron-sized first particles and a plurality of nano-sized second particles, and a binder; depositing the mixture onto a substrate to form a wetting-resistant surface via a thermal spray process. The mixture is deposited without substantial melting of the first and second particles. The wetting-resistant surface has wettability sufficient to generate, with a reference fluid, a static contact angle of greater than about 90 degrees.

Method of preparing wetting-resistant surfaces and articles incorporating the same

A target assembly for generating x-rays includes a target substrate, and an emissive coating attached to the target substrate, the emissive coating including a textured material including a plurality of granular protrusions arranged to increase gray body emissive characteristics of the target assembly above that of the target substrate.

Apparatus for increasing radiative heat transfer in an X-ray tube and method of making same

A target assembly for generating x-rays includes a target substrate, and an emissive coating applied to a portion of the target substrate, the emissive coating comprising one or more of a carbide and a carbonitride.

Apparatus for increasing radiative heat transfer in an x-ray tube and method of making same

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Delanson, NY, United States of America

Dennis Michael Gray