General Electric Company

Ge Infrastructure Technology, LLC

Cambridge Display Technology Limited

Momentive Performance Materials Gmbh

First Solar, Inc.

Anil Raj Duggal

Lionel M Levinson

Alok Mani Srivastava

Jie Jerry Liu

Joseph John Shiang

Larry Neil Lewis

Christian Maria Anton Heller

Minyoung Lee

Holly Ann Comanzo

Richard Louis Hart

Weijun Yin

Min Yan

Seung-Hyuck Hong

William Winder Beers

Honggang Wang

Donald Franklin Foust

Steven Jude Duclos

Marc Schaepkens

Michael Anthony Benjamin

Joseph Darryl Michael

Siegfried Aftergut

Ahmet Gun Erlat

Narendra Digamber Joshi

Herbert S Cole

Thomas Frederick Soules

David Arnold

Christopher P Yakymyshyn

Kelvin Ma

Larry Gene Turner

Richard J Saia

Paul Alan McConnelee

Daniel R Olson

Daniel Jason Erno

Hendrik Pieter Jacobus De Bock

Andrew Philip Shapiro

William Hullinger Huber

David Roger Moore

Hongyi Zhou

Frederic F Ahlgren

Thomas Francis McNulty

Benjamin Hale Winkler

Qin Chen

Kevin Warner Flanagan

Gautam Parthasarathy

Reza Sarrafi-Nour

Matthew Roberts

Clare Foden

Badri Narayan Ramamurthi

Oltea Puica Siclovan

Tae Won Kim

Chandra Sekher Yerramalli

Theresa Ann Sitnik-Nieters

Nalinkumar Lallubhai Patel

Andrew Joseph Wickersham

Michael Scott Herzog

Mark Leadbeater

Salvatore Cina

Mark Daniel Doherty

Larry Qiang Zeng

Donald Seton Farquhar

Craig Edward Murphy

Radislav Alexandrovich Potyrailo

Herman Wiegman

John M Davenport

Anant Achyut Setlur

James Anthony Cella

Hao Huang

William Dwight Gerstler

Bugra Han Ertas

John Frederick Ackerman

Lowell Scott Smith

Charles Burton Theurer

Raymond Albert Fillion

Ravisekhar Nadimpalli Raju

Yizhen Lin

Mohamed Rahmane

John Norton Park

Paul Michael Smigelski, Jr

Deepak Trivedi

Renato Guida

David Allan Torrey

Kyle Erik Litz

William Edward Burdick, Jr

Charles S Korman

Mario Ghezzo

Edward Brittain Stokes

Ernest Wayne Balch

Yung S Liu

Dennis Joseph Coyle

Mohandas Nayak

Ri-an Zhao

Wei Zhang

Kevin Henry Janora

Lili Zhang

Adam Fraser Halverson

Hongbo Cao

Qinglan Huang

Stefan Rakuff

Brian Joseph Scherer

Aharon Yakimov

A carbon dioxide (CO) capture system and method for removing COfrom an inlet gas including a first fluid stream inlet providing for the flow of a first fluid stream, such as an inlet gas containing CO, and a second fluid stream inlet providing for the flow of a second fluid stream, such as steam, an outlet providing for the flow of a COdepleted stream from the COcapture system, an outlet providing for the flow of a COstream from the COcapture system and a concentrator in fluid communication with the first fluid stream. The system further including a first contactor and a second contactor. Each of the first contactor and the second contactor defining therein a first fluidically-isolated, sorbent-integrated, fluid domain for flow of the first fluid stream and COadsorption and a second fluidically-isolated fluid domain for flow of the second fluid stream to assist in desorption.

Carbon dioxide capture with system of contactors each having fluidically-isolated, thermally-connected, parallel fluid domains

A combustion section defines an axial direction, a radial direction, and a circumferential direction. The combustion section includes a casing that defines a diffusion chamber. A combustion liner is disposed within the diffusion chamber and defines a combustion chamber the combustion liner is spaced apart from the casing such that a passageway is defined between the combustion liner and the casing. A fuel cell assembly is disposed in the passageway. The fuel cell assembly includes a fuel cell stack that has a plurality of fuel cells each extending between an inlet end and an outlet end. The inlet end receives a flow of air and fuel and the outlet end provides output products to the combustion chamber. The fuel cell assembly further includes an electrical circuit that is electrically coupled to the plurality of fuel cells and that extends through the casing.

Gas turbine combustion section having an integrated fuel cell assembly

A porous electrolyte structure for a solid state battery is provided. The porous electrolyte structure has an interconnected ceramic matrix with a network of open pores disposed throughout a thickness of the porous electrolyte structure. The porous electrolyte structure includes a porosity of about 20% by volume to about 80% by volume. A solid state battery cell including the porous electrolyte structure and a method of making the solid state battery cell are also provided.

Solid state battery, ceramic electrolyte structure and methods of making

An engine assembly includes a combustor, a fuel cell stack integrated with the combustor, and a pre-burner system fluidly connected to the fuel cell stack. The fuel cell stack is configured to direct fuel and air exhaust from the fuel cell stack into the combustor. The pre-burner system is configured to control a temperature of an air flow directed into the fuel cell stack. The combustor is configured to combust the fuel and air exhaust from the fuel cell stack into one or more gaseous combustion products that drive a downstream turbine. The engine assembly can further include a catalytic partial oxidation convertor that is fluidly connected to the fuel cell stack. The catalytic partial oxidation convertor is configured to develop a hydrogen rich fuel stream to be directed into the fuel cell stack.

Integrated fuel cell and engine combustor assembly

An engine assembly includes a combustor, a fuel cell stack integrated with the combustor, the fuel cell stack configured (i) to direct fuel and air exhaust from the fuel cell stack into the combustor and (ii) to generate electrical energy, a catalytic partial oxidation convertor that is fluidly connected to the fuel cell stack, the catalytic partial oxidation convertor being configured to optimize a hydrogen content of a fuel stream to be directed into the fuel cell stack, and one or more subsystems electrically connected with the fuel cell stack, the one or more subsystems being configured to receive the electrical energy generated by the fuel cell stack. The combustor is configured to combust the fuel and air exhaust from the fuel cell stack into one or more gaseous combustion products that drive a downstream turbine.

A combustion section defines an axial direction, a radial direction, and a circumferential direction. The combustion section includes a casing that defines a diffusion chamber. A combustion liner is disposed within the diffusion chamber and defines a combustion chamber. The combustion liner is spaced apart from the casing such that a passageway is defined between the combustion liner and the casing. A fuel cell assembly is disposed in the passageway. The fuel cell assembly includes a fuel cell that extends between an inlet end and an outlet end. The inlet end receives a flow of air and fuel and the outlet end provides output products to the combustion chamber. The fuel cell extends at an angle between the inlet end and the outlet end relative to a radial projection line.

Carbon dioxide capture system and method of capturing carbon dioxide

An article can include a ceramic insulator with an interior surface defining a recess, an insulator aperture in the interior surface, and an insulator cooling channel extending through at least a portion of the ceramic insulator to the insulator aperture. A first conductor can be at least partially disposed within the recess.

Articles including insulated conductors and systems thereof

A combustion section defines an axial direction, a radial direction, and a circumferential direction. The combustion section includes a casing that defines a diffusion chamber. A combustion liner is disposed within the diffusion chamber and defines a combustion chamber. The combustion liner is spaced apart from the casing such that a passageway is defined between the combustion liner and the casing. A fuel cell assembly is disposed in the passageway. The fuel cell assembly includes a fuel cell stack having a plurality of fuel cells each extending between an inlet end and an outlet end. Each fuel cell of the plurality of fuel cells includes an air channel and a fuel channel each fluidly coupled to the combustion chamber.

A combustion section defines an axial direction, a radial direction, and a circumferential direction. The combustion section includes a casing that defines a diffusion chamber. A combustion liner is disposed within the diffusion chamber and defines a combustion chamber. The combustion liner is spaced apart from the casing such that a passageway is defined between the combustion liner and the casing. A fuel cell assembly is disposed in the passageway. The fuel cell assembly includes a fuel cell stack that has a plurality of fuel cells each extending between an inlet end and an outlet end. The inlet end receives a flow of air and fuel and the outlet end provides output products to the combustion chamber. The outlet end of the plurality of fuel cells extends through the combustion liner and partially defines the combustion chamber.

A powered system that has an electric power system with a stator having plural poles with each pole having a conductive winding that may surround the corresponding pole and may be configured to generate a magnetic field, and a rotor that may be configured to rotate in response to the magnetic field generated by the stator. The at least one of the conductive windings may be insulated with an insulation material configured to conduct heat from the at least one conductive winding while operating at a temperature above 600&#xb0; C.

Electric power system for hypersonic speed operation

An electric machine includes a rotor assembly having a rotor core that extends in an axial direction and a stator assembly surrounding and coaxial with the rotor assembly. The stator assembly includes a stator core having slots extending in a radial direction into an inner surface of the stator core and extending axially from a first end surface to a second end surface of the stator core. The stator assembly includes stator coil windings disposed within the respective slots of the stator core and a first electrically insulating conformal coating disposed between the stator core and the stator coil windings. The conformal coating includes a polymer matrix impregnated with an effective amount of thermally conductive ceramic materials, above a percolation threshold, that form continuous thermal pathways across a thickness of the first coating.

Electrically insulating, thermally conductive coatings for electrical systems and deposition methods thereof

An article is presented. The article includes one or more ceramic insulators having a plurality of recesses including a first portion having a first set of recesses of the plurality of recesses and a second portion having a second set of recesses of the plurality of recesses. At least a portion of a first conductor and at least a portion of a first cooling channel are overlappingly disposed in a recess of the first set of recesses. At least a portion of a second conductor and at least a portion of a second cooling channel are disposed in at least one recess of the second set of recesses wherein the at least a portion of the second cooling channel offsets from the at least a portion of the second conductor. A system including the article is also presented.

A method includes forming one or more cores, wherein each of the one or more cores has a cross section corresponding to a conductor to be subsequently formed, forming an insulator around the one or more cores, removing the one or more cores to expose one or more recesses within the insulator, and forming one or more conductors in at least one of the one or more recesses of the insulator such that the cross sections of the one or more conductors conform to an interior surface of the one or more recesses in the insulator.

System of a conductor disposed within an insulator

This present disclosure generally relates to systems and methods of electrophoretic deposition (EPD) techniques for use in insulation systems at least partially encapsulating a semiconductor device, a conductive component and a substrate, such as insulation systems of semiconductor devices, busbars, or the like. Insulation systems formed using EPD processes may be designed to have a dielectric constant that decreases in a direction away from a substrate of the insulation system. This may improve insulation technologies since depositing coatings with sequentially arranged dielectric constants may improve resistance of the insulation system to high temperature, high electric fields, or the like.

Insulation systems and methods of depositing insulation systems

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Niskayuna, NY, United States of America

Anil Raj Duggal