The ammonia content of fuel gas in an IGCC power generation system is reduced through ammonia decomposition, thereby reducing the NO emissions from the plant. The power generation system includes a gasifier, a gas turbine and at least one catalytic reactor arranged between the gasifier and the gas turbine. The catalytic reactor may be either a three stage or two stage device. The three stage reactor includes a first catalyst which promotes water-gas-shift, a second catalyst which promotes CO methanation, and a third catalyst which promotes ammonia decomposition. The two stage reactor includes a first catalyst which promotes water-gas-shift and CO methanation and a second catalyst which promotes ammonia decomposition. The plural catalytic stages may be disposed in a single vessel or successively disposed in individual vessels, and the catalysts may be in a pelletized form or coated on honeycomb structures.
Fuel Composition And Method For Extending The Time Between Turbine Washes When Burning Ash Bearing Fuel In A Turbine
Alan S. Feitelberg - Niskayuna NY Vinod Kumar Pareek - Niskayuna NY Alan Whitehead - Charlton NY
Assignee:
General Electric Company - Schenectady NY
International Classification:
C10L 112
US Classification:
44370, 44457, 44458, 44603
Abstract:
The addition of a magnesium compound to an ash bearing fuel results in a reduction in the formation of deposits in the turbine and extending the interval between turbine washes when burning the ash bearing fuel in a turbine compared to burning the ash bearing fuel in a turbine without the addition of a magnesium compound. The additive is desirably effective with ash bearing fuel having less than 0. 5 ppm vanadium by weight, less than 1 ppm sodium and potassium combined by weight, and greater than about 25 ppm ash by weight or greater than 2 ppm calcium by weight. The additive is blended with the ash bearing fuel to give a mass ratio of magnesium to ash of between about 0. 5 to 1 and about 3 to 1, and desirably about 1 to 1 on a mass basis after mixing.
Gas Turbine Engine Combustor Can With Trapped Vortex Cavity
Joel Meier Haynes - Niskayuna NY Alan S. Feitelberg - Niskayuna NY David Louis Burrus - Cincinnati OH Narendra Digamber Joshi - Cincinnati OH
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 358
US Classification:
60746, 60750
Abstract:
A gas turbine engine combustor can downstream of a pre-mixer has a pre-mixer flowpath therein and circumferentially spaced apart swirling vanes disposed across the pre-mixer flowpath. A primary fuel injector is positioned for injecting fuel into the pre-mixer flowpath. A combustion chamber surrounded by an annular combustor liner disposed in supply flow communication with the pre-mixer. An annular trapped dual vortex cavity located at an upstream end of the combustor liner is defined between an annular aft wall, an annular forward wall, and a circular radially outer wall formed therebetween. A cavity opening at a radially inner end of the cavity is spaced apart from the radially outer wall. Air injection first holes are disposed through the forward wall and air injection second holes are disposed through the aft wall. Fuel injection holes are disposed through at least one of the forward and aft walls.
Gas Turbine Engine Combustor Can With Trapped Vortex Cavity
David Louis Burrus - Cincinnati OH, US Narendra Digamber Joshi - Cincinnati OH, US Joel Meier Haynes - Niskayuna NY, US Alan S. Feitelberg - Niskayuna NY, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F23R003/04
US Classification:
60746, 60750
Abstract:
A gas turbine engine combustor can downstream of a pre-mixer has a pre-mixer flowpath therein and circumferentially spaced apart swirling vanes disposed across the pre-mixer flowpath. A primary fuel injector is positioned for injecting fuel into the pre-mixer flowpath. A combustion chamber surrounded by an annular combustor liner disposed in supply flow communication with the pre-mixer. An annular trapped dual vortex cavity located at an upstream end of the combustor liner is defined between an annular aft wall, an annular forward wall, and a circular radially outer wall formed therebetween. A cavity opening at a radially inner end of the cavity is spaced apart from the radially outer wall. Air injection first holes are disposed through the forward wall and air injection second holes are disposed through the aft wall. Fuel injection holes are disposed through at least one of the forward and aft walls.
Ching-Jen Tang - Watervliet NY, US Alan S. Feitelberg - Niskayuna NY, US
Assignee:
Plug Power Inc. - Latham NY
International Classification:
H01M 8/04
US Classification:
429 17, 429 19, 429 34
Abstract:
An oxidizer that is usable with a fuel cell includes a catalyst, an inlet to communicate an oxidant flow, an injection tube to communicate an anode exhaust flow, a mixing tube and a divergent nozzle. The injection tube communicates the anode exhaust flow from the fuel cell into the oxidizer to produce a combined flow in which the anode exhaust flow is oriented in substantially the same direction as the oxidant flow and surrounded by the oxidant flow. The mixing tube is connected to the inlet to receive the combined flow and mix the oxidant flow and the anode exhaust flow mix together to produce a mixed flow. A cross-sectional flow area of the mixing tube is sized to prevent flashback. The divergent nozzle communicates the mixed flow to the catalyst.
Parshant Dhand - Troy NY, US Troy Scriven - Waterford NY, US Richard Graham - Scotia NY, US David Parry - Clifton Park NY, US Alan Feitelberg - Niskayuna NY, US
International Classification:
F01N 3/20 H01M 8/06 H01M 8/04
US Classification:
422105000, 429019000, 429025000
Abstract:
A fuel cell system includes a de-sulfurization tank, a reformer, a pressure monitoring device and a fuel cell stack. The de-sulfurization tank includes an agent that is adapted to remove sulfur compounds and is capable of undergoing a conditioning cycle. The tank includes an inlet to receive a first hydrocarbon flow and an outlet to provide a second hydrocarbon flow. The reformer is adapted to convert the second hydrocarbon flow into a reformate flow, which is received by the fuel cell stack. The pressure monitoring device monitors a pressure of the second hydrocarbon flow, a circuit of the fuel cell system is coupled to the pressure monitoring device to determine whether the conditioning of the tank is complete based on the pressure.
Detecting And Controlling A Fuel-Rich Condition Of A Reactor In A Fuel Cell System
Vishnu L. Poonamallee - Tamilnadu, IN Zhi Zhou - Selkirk NY, US Parshant Dhand - Lansdale PA, US Alan S. Feitelberg - Niskayuna NY, US
International Classification:
H01M 8/04
US Classification:
429 17, 429 34
Abstract:
A fuel cell system includes a fuel cell stack, and a reactor to oxidize excess fuel exhausted from the fuel cell stack. A sensor associated with the reactor provides an output indication, and a controller detects a fuel-rich condition of the reactor based on the output indication from the sensor.
Alan S. Feitelberg - Niskayuna NY Kevin Michael Elward - Simpsonville SC Robert Lee Hillis - Oneonta NY Milton Bradford Hilt - Sloansville NY John Francis Love - Slingerlands NY Roointon Erach Pavri - Schenectady NY Richard Benjamin Schiefer - Niskayuna NY Richard Arthur Symonds - Simpsonville SC
Assignee:
General Electric Company - Schnectady NY
International Classification:
F02C 300
US Classification:
60752
Abstract:
An optimized combustor cooperating with a compressor in driving a gas turbine comprises a cylindrical outer combustor wall having an upstream fuel entry region and a downstream turbine entry region. An array of mixing holes are disposed about the periphery of the outer combustor wall adjacent to the fuel entry region so as to lower No. sub. x production therein. An array of dilution holes are medially disposed within the outer combustor wall to provide an entry for dilution air to the combustor.
Cornell University Nov 1, 2012 - Dec 2018
Senior Lecturer
Iogen Corporation May 2009 - May 2012
Senior Manager, Technology Demonstration
Iogen Corporation Nov 2008 - May 2009
Manager, Process Research and Development
Plug Power Sep 2001 - Jun 2008
Director, Advanced Concepts
Clarkson University Capital Region Campus Aug 2004 - Dec 2004
Adjunct Faculty
Education:
Shrewsbury High School 2016 - 2020
Massachusetts Institute of Technology 1984 - 1990
Master of Science, Doctorates, Masters, Doctor of Philosophy, Chemical Engineering
Worcester Polytechnic Institute 1980 - 1984
Bachelors, Bachelor of Science, Chemical Engineering
Shrewsbury High School 1978 - 1980
Skills:
Combustion Fuel Cells Thermodynamics Aspen Plus Chemical Engineering Energy Six Sigma Dmaic Taguchi Methods Design of Experiments Process Engineering R&D Biofuels Product Development Characterization Manufacturing Engineering Cross Functional Team Leadership Process Simulation Materials Science Process Optimization Continuous Improvement