Patents by Inventor Alston Ilford Scipio
Alston Ilford Scipio has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 12287095Abstract: A method of blending at least two fuels includes providing at least two fuels to a cyclonic mixer via a fuel supply system, the fuel supply system including a fuel supply circuit for each fuel of the at least two fuels, mixing, via at least one vortex formed in the cyclonic mixer, the at least two fuels to form a fuel mixture, determining, via one or more sensors, a measured interchangeability index of the fuel mixture, comparing the measured interchangeability index to a predetermined interchangeability index, adjusting, via the fuel supply system, one or more parameters of at least one of the at least two fuels based on the comparison between the measured interchangeability index and the predetermined interchangeability index, and providing the fuel mixture to a combustion system.Type: GrantFiled: June 5, 2024Date of Patent: April 29, 2025Assignee: GE Infrastructure Technology LLCInventors: Colin Noel Stevens, Temitayo O. Femi-Fowode, Adenuga Moshood Adelakun, Alston Ilford Scipio, Oyebimpe B. Olubode, John Karigiannis
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Patent number: 12281590Abstract: A lift system and method for installation and removal of a combustion can from a turbomachine are provided. The lift system includes a rail, a portable cart assembly, and a slide assembly. The portable cart assembly includes a combustion can cradle assembly coupled to a telescopic member. The combustion can cradle assembly is configured to removably couple to a combustion can of the turbomachine. The slide assembly is removably couplable to the portable cart assembly and the rail. The slide assembly is movable with the portable cart assembly along the rail to adjust a position of the combustion can cradle assembly.Type: GrantFiled: June 29, 2022Date of Patent: April 22, 2025Assignee: GE Infrastructure Technology LLCInventors: Humberto Sanchez Moreno, Artemio Josue Aguilar Cuellar, Juan Daniel Mendez Rodriguez, Alston Ilford Scipio
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Patent number: 12281620Abstract: A method of blending at least two fuels includes providing at least two fuels to a helical static mixer via a fuel supply system, the fuel supply system including a fuel supply circuit for each fuel of the at least two fuels, mixing, via a plurality of helical structures of the helical static mixer, the at least two fuels to form a fuel mixture, determining, via one or more sensors, a measured interchangeability index of the fuel mixture, comparing the measured interchangeability index to a predetermined interchangeability index, adjusting, via the fuel supply system, one or more parameters of at least one of the at least two fuels based on the comparison between the measured interchangeability index and the predetermined interchangeability index, and providing the fuel mixture to a combustion system.Type: GrantFiled: June 5, 2024Date of Patent: April 22, 2025Assignee: GE Infrastructure Technology LLCInventors: Temitayo O. Femi-Fowode, Alston Ilford Scipio, Adenuga Moshood Adelakun, Oyebimpe B. Olubode, Colin Noel Stevens, John Karigiannis
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Publication number: 20240003269Abstract: A lift system and method for installation and removal of a combustion can from a turbomachine are provided. The lift system includes a rail, a portable cart assembly, and a slide assembly. The portable cart assembly includes a combustion can cradle assembly coupled to a telescopic member. The combustion can cradle assembly is configured to removably couple to a combustion can of the turbomachine. The slide assembly is removably couplable to the portable cart assembly and the rail. The slide assembly is movable with the portable cart assembly along the rail to adjust a position of the combustion can cradle assembly.Type: ApplicationFiled: June 29, 2022Publication date: January 4, 2024Inventors: Humberto Sanchez Moreno, Artemio Josue Aguilar Cuellar, Juan Daniel Mendez Rodriguez, Alston Ilford Scipio
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Patent number: 11859533Abstract: A gas turbine engine system includes a gas turbine engine including a compressor, combustor including a plurality of late lean fuel injectors supplied with secondary fuel; gas turbine, and wash system configured to be attached and in fluid communication with the late lean fuel injectors. The wash system includes a water source including water; first fluid source including a first fluid providing vanadium ash and vanadium deposit mitigation and removal from internal gas turbine components; a mixing chamber in communication with the water source and first fluid source; a water pump to pump the water to the mixing chamber; a first fluid pump the first fluid to the mixing chamber; a fluid line in fluid communication with the mixing chamber and late lean fuel injectors so fluid from the mixing chamber is injected into the combustor at the late lean fuel injectors while the gas turbine engine is on-line.Type: GrantFiled: June 3, 2021Date of Patent: January 2, 2024Assignee: General Electric CompanyInventors: Alston Ilford Scipio, Sanji Ekanayake
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Patent number: 11814972Abstract: A system comprises a gas turbine engine including a compressor, combustor, gas turbine, the combustor including a plurality of late lean fuel injectors; and wash system configured to be attached to and in fluid communication with the a plurality of late lean fuel injectors of the combustor. The wash system includes a water source supplying water; a first fluid source supplying a first fluid; a mixing chamber in communication with the water source and first fluid source; a water pump to pump water to the mixing chamber; a first fluid pump to pump the first fluid to the mixing chamber; a fluid line in fluid communication with the mixing chamber and at least one of the plurality of late lean fuel injectors so fluid from the mixing chamber is injected into the combustor at late lean fuel injectors. The wash system is operated with the gas turbine engine off-line.Type: GrantFiled: June 3, 2021Date of Patent: November 14, 2023Assignee: General Electric CompanyInventors: Alston Ilford Scipio, Justin Todd Eggart, Colin Noel Stevens, Sanji Ekanayake
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Patent number: 11773772Abstract: A system includes an annular track that surrounds the turbomachine. The annular track includes an upper rail portion and a lower rail portion removably coupled to one another. The system further includes a drive assembly operably coupled to the annular track. The drive assembly includes a drive chain that extends along the annular track. The system further includes a plurality of carts rotatably coupled to the annular track and connected to the drive chain such that operation of the drive assembly alters a circumferential position of the plurality of carts with respect to an axial centerline of the turbomachine. The system further includes a plurality of combustion can cradle assemblies each coupled to a respective cart of the plurality of carts. Each combustion can cradle assembly of the plurality of combustion can cradle assemblies is configured to removably couple to a combustion can of the one or more combustion cans.Type: GrantFiled: July 19, 2021Date of Patent: October 3, 2023Assignee: General Electric CompanyInventors: Artemio Josue Aguilar Cuéllar, Humberto Sanchez Moreno, Alston Ilford Scipio
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Publication number: 20230115387Abstract: A gas turbine engine system includes a compressor, gas turbine, and combustor including a plurality of late lean fuel injectors supplied with secondary fuel to its interior. The gas turbine engine system includes a wash system in communication with the late lean fuel injectors. The wash system includes a water source; water pump; anti-corrosion agent fluid source with an anti-corrosion agent including a amine corrosion inhibitor; anti-corrosion agent supply piping in fluid communication with the anti-corrosion agent fluid source; mixing chamber receiving water and anti-corrosion agent to produce an anti-corrosion mixture in fluid communication with the mixing chamber and the plurality of late lean fuel injectors. Fluid from the mixing chamber including the water, the anti-corrosion agent fluid source, or a mixture thereof is injected, while the gas turbine engine is off-line, into the combustor and at least one of the plurality of late lean fuel injectors.Type: ApplicationFiled: December 14, 2022Publication date: April 13, 2023Inventors: Alston Ilford Scipio, Colin Noel Stevens, Sanji Ekanayake
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Publication number: 20230034885Abstract: A method for inhibiting particulate ingress in a combustion system includes acquiring particulate ingress data, determining a probable particulate ingress location on an air inlet of the combustion system in dependence upon the particulate ingress data, and deploying a filter screen at the determined probable particulate ingress location to inhibit particulate ingress at the determined probable particulate ingress location.Type: ApplicationFiled: July 28, 2021Publication date: February 2, 2023Applicant: GENERAL ELECTRIC COMPANYInventors: MARUTHI MANOHAR JUPUDI, ALSTON ILFORD SCIPIO, MALLAREDDY SOUDARY, JUERGEN GERHARD HOFFMANN
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Publication number: 20230033140Abstract: A control system for turbine systems configured to provide accurate interpretations of detected particle accumulation, improve performance of turbine systems, and/or minimize costs due to downtime and maintenance are disclosed. The control system may build an intelligent model of fluid flow based on measured data provided by a sensor in a fluid flow path of the turbine system. The intelligent model consults a filter efficiency framework and determines an impact value that quantifies an operational efficiency of the turbine system and may identify a location of possible leakage, estimate a total amount of ingress of particles, identify components of the turbine system that may be operating in a diminished capacity, estimate a risk of damage to components of the turbine system, and/or recommend mitigation actions.Type: ApplicationFiled: July 28, 2021Publication date: February 2, 2023Applicant: GENERAL ELECTRIC COMPANYInventors: MARUTHI MANOHAR JUPUDI, KAMEL ABDELKADER TAYEBI, ABDURRAHMAN ABDALLAH KHALIDI, JOSE ANTONIO CUEVAS ALVAREZ, ALSTON ILFORD SCIPIO, BRADLY AARON KIPPEL
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Publication number: 20230018703Abstract: A system includes an annular track that surrounds the turbomachine. The annular track includes an upper rail portion and a lower rail portion removably coupled to one another. The system further includes a drive assembly operably coupled to the annular track. The drive assembly includes a drive chain that extends along the annular track. The system further includes a plurality of carts rotatably coupled to the annular track and connected to the drive chain such that operation of the drive assembly alters a circumferential position of the plurality of carts with respect to an axial centerline of the turbomachine. The system further includes a plurality of combustion can cradle assemblies each coupled to a respective cart of the plurality of carts. Each combustion can cradle assembly of the plurality of combustion can cradle assemblies is configured to removably couple to a combustion can of the one or more combustion cans.Type: ApplicationFiled: July 19, 2021Publication date: January 19, 2023Inventors: Artemio Josue Aguilar Cuéllar, Humberto Sanchez Moreno, Alston Ilford Scipio
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Patent number: 11555447Abstract: A method for inhibiting particulate ingress in a combustion system includes acquiring particulate ingress data, determining a probable particulate ingress location on an air inlet of the combustion system in dependence upon the particulate ingress data, and deploying a filter screen at the determined probable particulate ingress location to inhibit particulate ingress at the determined probable particulate ingress location.Type: GrantFiled: July 28, 2021Date of Patent: January 17, 2023Assignee: GENERAL ELECTRIC COMPANYInventors: Maruthi Manohar Jupudi, Alston Ilford Scipio, Mallareddy Soudary, Juergen Gerhard Hoffmann
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Patent number: 11555415Abstract: A gas turbine engine system includes a compressor, gas turbine, and combustor including a plurality of late lean fuel injectors supplied with secondary fuel to its interior. The gas turbine engine system includes a wash system in communication with the late lean fuel injectors. The wash system includes a water source; water pump; anti-corrosion agent fluid source with an anti-corrosion agent including a polyamine corrosion inhibitor; anti-corrosion agent supply piping in fluid communication with the anti-corrosion agent fluid source; mixing chamber receiving water and anti-corrosion agent to produce an anti-corrosion mixture in fluid communication with the mixing chamber and the plurality of late lean fuel injectors. Fluid from the mixing chamber including the water, the anti-corrosion agent fluid source, or a mixture thereof is injected, while the gas turbine engine is off-line, into the combustor at at least one of the plurality of late lean fuel injectors.Type: GrantFiled: June 3, 2021Date of Patent: January 17, 2023Assignee: General Electric CompanyInventors: Alston Ilford Scipio, Colin Noel Stevens, Sanji Ekanayake
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Publication number: 20220389833Abstract: A gas turbine engine system includes a compressor, gas turbine, and combustor including a plurality of late lean fuel injectors supplied with secondary fuel to its interior. The gas turbine engine system includes a wash system in communication with the late lean fuel injectors. The wash system includes a water source; water pump; anti-corrosion agent fluid source with an anti-corrosion agent including a polyamine corrosion inhibitor; anti-corrosion agent supply piping in fluid communication with the anti-corrosion agent fluid source; mixing chamber receiving water and anti-corrosion agent to produce an anti-corrosion mixture in fluid communication with the mixing chamber and the plurality of late lean fuel injectors. Fluid from the mixing chamber including the water, the anti-corrosion agent fluid source, or a mixture thereof is injected, while the gas turbine engine is off-line, into the combustor at at least one of the plurality of late lean fuel injectors.Type: ApplicationFiled: June 3, 2021Publication date: December 8, 2022Inventors: Alston Ilford Scipio, Colin Noel Stevens, Sanji Ekanayake
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Publication number: 20220389832Abstract: A system comprises a gas turbine engine including a compressor, combustor, gas turbine, the combustor including a plurality of late lean fuel injectors; and wash system configured to be attached to and in fluid communication with the a plurality of late lean fuel injectors of the combustor. The wash system includes a water source supplying water; a first fluid source supplying a first fluid; a mixing chamber in communication with the water source and first fluid source; a water pump to pump water to the mixing chamber; a first fluid pump to pump the first fluid to the mixing chamber; a fluid line in fluid communication with the mixing chamber and at least one of the plurality of late lean fuel injectors so fluid from the mixing chamber is injected into the combustor at late lean fuel injectors. The wash system is operated with the gas turbine engine off-line.Type: ApplicationFiled: June 3, 2021Publication date: December 8, 2022Inventors: Alston Ilford Scipio, Justin Todd Eggart, Colin Noel Stevens, Sanji Ekanayake
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Publication number: 20220389863Abstract: A gas turbine engine system includes a gas turbine engine including a compressor, combustor including a plurality of late lean fuel injectors supplied with secondary fuel; gas turbine, and wash system configured to be attached and in fluid communication with the late lean fuel injectors. The wash system includes a water source including water; first fluid source including a first fluid providing vanadium ash and vanadium deposit mitigation and removal from internal gas turbine components; a mixing chamber in communication with the water source and first fluid source; a water pump to pump the water to the mixing chamber; a first fluid pump the first fluid to the mixing chamber; a fluid line in fluid communication with the mixing chamber and late lean fuel injectors so fluid from the mixing chamber is injected into the combustor at the late lean fuel injectors while the gas turbine engine is on-line.Type: ApplicationFiled: June 3, 2021Publication date: December 8, 2022Inventors: Alston Ilford Scipio, Sanji Ekanayake
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Patent number: 11492929Abstract: A lift assembly includes an upper rail. A plurality of rail flanges extend from the upper rail. The lift assembly further includes a plurality of combustion can support assemblies spaced apart from one another. Each combustion can support assembly of the plurality of combustion can support assemblies includes a support flange slidably coupled to a rail flange of the plurality of rail flanges, an outer sleeve, and an inner sleeve assembly configured to removably couple to a combustion can of the turbomachine. Each combustion can support assembly of the plurality of combustion can support assemblies defines a cylindrical coordinate system having an axial direction, a radial direction, and a circumferential direction. Each combustion can support assembly of the plurality of support assemblies is configured to move along any of the axial direction, the radial direction, or the circumferential direction relative to the upper rail.Type: GrantFiled: July 19, 2021Date of Patent: November 8, 2022Assignee: General Electric CompanyInventors: Artemio Josue Aguilar Cuéllar, Benigno Camacho Mendoza, Alejandro Perez, Alston Ilford Scipio
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Patent number: 11365677Abstract: A combined cycle power plant that includes a first gas turbine engine including a first turbine section, a second gas turbine engine including a second turbine section having an aft outlet configured to discharge an exhaust gas stream, an emissions reduction system configured to receive the exhaust gas stream discharged from the second gas turbine engine, and configured to remove oxides of nitrogen from the exhaust gas stream, and an interstage extraction system communicatively coupled with the first turbine section. The interstage extraction system is configured to selectively extract turbine extraction air from the first turbine section for providing heat to the emissions reduction system.Type: GrantFiled: March 25, 2020Date of Patent: June 21, 2022Assignee: GENERAL ELECTRIC COMPANYInventors: Joseph Klosinski, Sanji Ekanayake, Alston Ilford Scipio, George Vargese Mathai
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Publication number: 20210301686Abstract: A combined cycle power plant that includes a first gas turbine engine including a first turbine section, a second gas turbine engine including a second turbine section having an aft outlet configured to discharge an exhaust gas stream, an emissions reduction system configured to receive the exhaust gas stream discharged from the second gas turbine engine, and configured to remove oxides of nitrogen from the exhaust gas stream, and an interstage extraction system communicatively coupled with the first turbine section. The interstage extraction system is configured to selectively extract turbine extraction air from the first turbine section for providing heat to the emissions reduction system.Type: ApplicationFiled: March 25, 2020Publication date: September 30, 2021Inventors: Joseph Klosinski, Sanji Ekanayake, Alston Ilford Scipio, George Vargese Mathai
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Patent number: 10975774Abstract: The present application provides a gas turbine engine. The gas turbine engine may include a compressor, a compressor wash system in communication with the compressor, a condensate or boiler feed water system in communication with the compressor, and a dosing system in communication with the condensate or boiler feed water system.Type: GrantFiled: December 16, 2014Date of Patent: April 13, 2021Assignee: GENERAL ELECTRIC COMPANYInventors: Alston Ilford Scipio, Paul Robert Fernandez, Rebecca Evelyn Hefner, Sanji Ekanayake