Patents by Inventor Arthur Williams
Arthur Williams 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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Publication number: 20240133318Abstract: A gas turbine engine, comprising a turbomachine and a housing at least partially encasing a portion of the turbomachine, the housing having an inner surface and defining in part a void between the inner surface and the portion of the turbomachine, the housing moveable relative to the portion of the turbomachine; and an engine component selectively coupled to the portion of the turbomachine or to the housing.Type: ApplicationFiled: October 24, 2022Publication date: April 25, 2024Inventors: Brian Lewis Devendorf, Arthur William Sibbach
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Patent number: 11965424Abstract: A method for providing overspeed protection for a gas turbine engine having an engine shaft includes monitoring, via an overspeed protection system, a torque of the engine shaft. The method also includes determining, via the overspeed protection system, at least one additional condition of the engine shaft. Further, the method includes determining, via the overspeed protection system, an overspeed condition of the gas turbine engine when the torque of the engine shaft drops below a torque threshold and the at least one additional condition of the engine shaft is indicative of the gas turbine engine being in an operational state. Thus, the overspeed condition is indicative of an above normal rotational speed of the engine shaft. In addition, the method includes initiating a shutdown procedure for the gas turbine engine in response to the determined overspeed condition to reduce the rotational speed of the engine shaft.Type: GrantFiled: June 21, 2022Date of Patent: April 23, 2024Assignee: General Electric CompanyInventors: Arthur William Sibbach, Brandon Wayne Miller, Erich Alois Krammer, Douglas Scott Jacobs, Joseph Alfred Iannotti
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Publication number: 20240110522Abstract: A gas turbine engine includes a rotatably driven engine component including a shaft coupling. The shaft coupling defines a first axial centerline and includes an inner surface. The inner surface includes a plurality of internal splines extending radially inwardly from the inner surface with respect to the first axial centerline. The engine further includes a driving member having a driving end portion and defining a second axial centerline. The driving end portion includes an outer surface and a plurality of external splines extending radially outwardly from the outer surface with respect to the second axial centerline. The plurality of external splines is drivingly engaged with the plurality of internal splines. The plurality of internal splines or the plurality of external splines comprises bowed splines.Type: ApplicationFiled: October 4, 2022Publication date: April 4, 2024Inventors: Arthur William Sibbach, Brandon Wayne Miller, Andrew Hudecki
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Publication number: 20240103184Abstract: A method for global navigation satellite system (GNSS)-based navigation may include retrieving terrain data for a geographical region and satellite orbit data for a GNSS comprising a plurality of satellites. Then, for of a plurality of time steps in a time period and for each of a plurality of lateral positions in the geographic region, a minimum height at which each satellite is visible from the lateral position at the time step may be determined. Unique combinations of satellites visible from the lateral position at the time step may be identified and error objects indicating GNSS performance quality corresponding to the unique combination of satellites may be generated. Performance quality information may be produced based on the one or more unique combinations of satellites and the respective one or more error objects. At least one aircraft may be operated based on this performance quality information.Type: ApplicationFiled: September 15, 2023Publication date: March 28, 2024Applicants: The MITRE Corporation, NASA Langley Research CenterInventors: Arthur K. SCHOLZ, Emily V. Bates, Kenneth William Schmitt, Evan Tyler Dill, Julian Gutierrez
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Patent number: 11941140Abstract: Various techniques are described for platform management of integrated access of public and privately-accessible datasets utilizing federated query generation and query schema rewriting optimization, including receiving at a dataset access platform a query formatted according to a first data schema, generating a copy of the query, saving the query and the copy to a datastore, parsing the copy of the query in the first schema using an inference engine, determining whether the query comprises data associated with an access control condition associated with accessing the dataset, the access control condition being configured to indicate whether the query is permitted to access the dataset, and rewriting, using a proxy server, the copy of the query in a second schema, and optimizing the rewriting by identifying a database engine to execute the query and including other data converted into another triple associated with an attribute of the query.Type: GrantFiled: June 30, 2022Date of Patent: March 26, 2024Assignee: data.world, Inc.Inventors: Bryon Kristen Jacob, David Lee Griffith, Triet Minh Le, Shad William Reynolds, Arthur Albert Keen
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Patent number: 11928596Abstract: Various techniques are described for platform management of integrated access of public and privately-accessible datasets utilizing federated query generation and query schema rewriting optimization, including receiving at a dataset access platform a query formatted according to a first data schema, generating a copy of the query, saving the query and the copy to a datastore, parsing the copy of the query in the first schema using an inference engine, determining whether the query comprises data associated with an access control condition associated with accessing the dataset, the access control condition being configured to indicate whether the query is permitted to access the dataset, and rewriting, using a proxy server, the copy of the query in a second schema by converting the copy of the query into a triple associated with the query and another triple associated with the access control condition.Type: GrantFiled: May 31, 2022Date of Patent: March 12, 2024Assignee: data.world, Inc.Inventors: Bryon Kristen Jacob, David Lee Griffith, Triet Minh Le, Shad William Reynolds, Arthur Albert Keen
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Publication number: 20240076180Abstract: A beverage production system, comprising a cup dispensing station configured to dispense cups, a beverage dispensing station configured to dispense a beverage, and a turntable assembly. The turntable assembly comprising a central axis, an inner turntable including a first row of cup receptacles, and an outer turntable including a second row of cup receptacles. The outer turntable is disposed circumferentially about the inner turntable, and the outer turntable is configured to rotate about the central axis to align the cup receptacles of the second row with the cup dispensing station and the beverage dispensing station. The turntable assembly is configured to align an opening in a cup receptacle in the second row with an opening in a cup receptacle in the first row. A slide assembly includes an arm configured to slide a cup positioned in the cup receptacle in the second row into the aligned opening of the cup receptacle in the first row.Type: ApplicationFiled: November 13, 2023Publication date: March 7, 2024Inventors: Nicholas Michael Degnan, Arthur Francois David Levy, Robert William Lyle, Joseph Park, Aaron Thomas, Karl Thomas Szatrowski, Won Suk You, Elvis Junior Palma, Sze Wun Wong
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Patent number: 11900233Abstract: In example embodiments, a method of interactive imitation learning method is disclosed. An input is received from an input device. The input includes data describing a first set of example actions defining a behavior for a virtual character. Inverse reinforcement learning is used to estimate a reward function for the set of example actions. The reward function and the set of example actions is used as input to a reinforcement learning model to train a machine learning agent to mimic the behavior in a training environment. Based on a measure of failure of the training of the machine learning agent reaching a threshold, the training of the machine learning agent is paused to request a second set of example actions from the input device. The second set of example actions is used in addition to the first set of example actions to estimate a new reward function.Type: GrantFiled: May 26, 2022Date of Patent: February 13, 2024Assignee: Unity IPR ApSInventors: Arthur William Juliani, Jr., Mohamed Marwan A. Mattar
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Publication number: 20240026901Abstract: A gas turbine engine includes a fan having a plurality of fan blades, a turbomachine operably coupled to the fan for driving the fan, the turbomachine including a compressor section, a combustion section, and a turbine section in serial flow order and together defining a core air flowpath, a nacelle surrounding and at least partially enclosing the fan, the nacelle defining a longitudinal axis, and an inlet pre-swirl feature located upstream of the plurality of fan blades, the inlet pre-swirl feature attached to or integrated into the nacelle, wherein the inlet pre-swirl feature is transitionable between a first angle with respect to the longitudinal axis of the nacelle and a second angle with respect to the longitudinal axis of the nacelle.Type: ApplicationFiled: October 5, 2023Publication date: January 25, 2024Inventors: Brandon Wayne Miller, Arthur William Sibbach
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Publication number: 20240011417Abstract: A pericritical fluid system for a thermal management system associated with a turbine engine may include one or more sensors configured to generate sensor outputs corresponding to one or more phase properties of a pericritical fluid flowing through a cooling circuit of the thermal management system, and a controller configured to generate control commands configured to control one or more controllable components of the thermal management system based at least in part on the sensor outputs. The one or more sensors may include one or more phase detection sensors, such as an acoustic sensor.Type: ApplicationFiled: September 6, 2023Publication date: January 11, 2024Inventors: Arthur William Sibbach, Aaron Michael Dziech, Scott Alan Schimmels, Robert R. Rachedi, Jeffrey Douglas Rambo, Brandon Wayne Miller
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Publication number: 20240003294Abstract: A turbofan engine is provided. The turbofan engine includes a fan comprising a plurality of fan blades; a turbomachine operably coupled to the fan for driving the fan, the turbomachine comprising a compressor section, a combustion section, and a turbine section in serial flow order and together defining a core air flowpath; a nacelle surrounding and at least partially enclosing the fan; an inlet pre-swirl feature located upstream of the plurality of fan blades, the inlet pre-swirl feature attached to or integrated into the nacelle; and a means for reducing ice buildup or ice formation on the inlet pre-swirl feature, the means in communication with the inlet pre-swirl feature.Type: ApplicationFiled: July 17, 2023Publication date: January 4, 2024Inventors: Arthur William Sibbach, Allan George van de Wall, Sean Christopher Binion, Brian Lewis Devendorf, Brandon Wayne Miller
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Publication number: 20230407795Abstract: A shaft power transfer system includes a first mechanical clutch mechanism operably coupling a high-pressure shaft to a low-pressure shaft. The first mechanical clutch mechanism transfers power from the high-pressure shaft to the low-pressure shaft at a predefined first speed transient condition. The system further includes a second mechanical clutch mechanism that operably couples the low-pressure shaft to the high-pressure shaft. The second mechanical clutch mechanism transfers power from the low-pressure shaft to the high-pressure shaft at a predefined second speed transient condition where the predefined first speed transient condition is different than the predefined second speed transient condition.Type: ApplicationFiled: June 21, 2022Publication date: December 21, 2023Inventors: Arthur William Sibbach, Brandon Wayne Miller, Jeffrey Douglas Rambo
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Publication number: 20230407761Abstract: A method for providing overspeed protection for a gas turbine engine having an engine shaft includes monitoring, via an overspeed protection system, a torque of the engine shaft. The method also includes determining, via the overspeed protection system, at least one additional condition of the engine shaft. Further, the method includes determining, via the overspeed protection system, an overspeed condition of the gas turbine engine when the torque of the engine shaft drops below a torque threshold and the at least one additional condition of the engine shaft is indicative of the gas turbine engine being in an operational state. Thus, the overspeed condition is indicative of an above normal rotational speed of the engine shaft. In addition, the method includes initiating a shutdown procedure for the gas turbine engine in response to the determined overspeed condition to reduce the rotational speed of the engine shaft.Type: ApplicationFiled: June 21, 2022Publication date: December 21, 2023Inventors: Arthur William Sibbach, Brandon Wayne Miller, Erich Alois Krammer, Douglas Scott Jacobs, Joseph Alfred Iannotti
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Patent number: 11833779Abstract: A coated component having a composite substrate and a coating system disposed thereon is provided. The coating system is substantially non-porous such that hydrocarbon fuel or other carbonaceous fluids are prevented from contacting and impregnating the polymer matrix composite material. The coating system can include an aluminum layer or a film layer comprising a polyethylene film or a polypropylene film. Also provided is a composite fan casing for a gas turbine engine having a polymer matrix composite substrate and a coating system disposed thereon. Methods for forming a containment assembly of a gas turbine engine are provided.Type: GrantFiled: November 20, 2020Date of Patent: December 5, 2023Assignee: General Electric CompanyInventors: Arthur William Sibbach, Wendy Wenling Lin
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Publication number: 20230378827Abstract: An airgap cooling system (140) for an electric machine (100), the electric machine (100) including a rotor assembly (102) rotatably mounted within a stator assembly (120) and defining an airgap (130) therebetween, wherein the stator assembly (120) comprises a lamination stack (124). The airgap cooling system (140) includes a plurality of distribution passages (142) that extend through the lamination stack (124); a plurality of discharge passages (150) that extend between the plurality of distribution passages (142) and the airgap (130); a cooling manifold (160) defining an annular distribution plenum (164) in fluid communication with the plurality of distribution passages (142), wherein the cooling manifold (160) is configured for receiving a cooling fluid (144) and directing the cooling fluid (144) into the distribution plenum (164), through the distribution passage (142) and the discharge passage (150), and into the airgap (130).Type: ApplicationFiled: December 21, 2022Publication date: November 23, 2023Inventors: Bugra Han Ertas, Joseph John Zierer, JR., Vandana Prabhakar Rallabandi, David Allan Torrey, David William Crall, Mohamed Osama, Adam Tomasz Pazinski, Arthur William Sibbach
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Patent number: 11808281Abstract: A gas turbine engine includes a fan having a plurality of fan blades, a turbomachine operably coupled to the fan for driving the fan, the turbomachine including a compressor section, a combustion section, and a turbine section in serial flow order and together defining a core air flowpath, a nacelle surrounding and at least partially enclosing the fan, the nacelle defining a longitudinal axis, and an inlet pre-swirl feature located upstream of the plurality of fan blades, the inlet pre-swirl feature attached to or integrated into the nacelle, wherein the inlet pre-swirl feature is transitionable between a first angle with respect to the longitudinal axis of the nacelle and a second angle with respect to the longitudinal axis of the nacelle.Type: GrantFiled: March 4, 2022Date of Patent: November 7, 2023Assignee: General Electric CompanyInventors: Brandon Wayne Miller, Arthur William Sibbach
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Publication number: 20230332513Abstract: A method of regulating pressure in a thermal transport bus of a gas turbine engine, the method including: operating the gas turbine engine with the thermal transport bus having an intermediary heat exchange fluid flowing therethrough, the thermal transport bus including one or more heat source heat exchangers and one or more heat sink heat exchangers in thermal communication through the intermediary heat exchanger fluid; and adjusting a flow volume of the thermal transport bus using a variable volume device in fluid communication with the thermal transport bus in response to a pressure change associated with the thermal transport bus.Type: ApplicationFiled: June 6, 2023Publication date: October 19, 2023Inventors: Scott Alan Schimmels, Daniel Alan Niergarth, Arthur William Sibbach, Brandon Wayne Miller
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Patent number: 11788465Abstract: A gas turbine engine comprises a turbomachine defining a core flow therethrough during operation. A flow tap is provided in fluid communication with the turbomachine, wherein the flow tap is configured to receive a portion of the core flow therethrough as a bleed flow. A bleed assembly includes a machine load, a bleed flow machine, and a bleed regulator. The bleed flow machine is disposed in fluid communication with the turbomachine through the flow tap, and is configured to drive the machine load. The bleed regulator is configured to regulate a bleed output provided to the bleed flow machine by controlling a capture rate of the bleed flow by the bleed flow machine.Type: GrantFiled: January 19, 2022Date of Patent: October 17, 2023Assignee: General Electric CompanyInventors: Brandon Wayne Miller, Patrick Michael Marrinan, Arthur William Sibbach, Scott Alan Schimmels, Scott David Hunter
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Patent number: 11788474Abstract: A pericritical fluid system for a thermal management system associated with a turbine engine may include one or more sensors configured to generate sensor outputs corresponding to one or more phase properties of a pericritical fluid flowing through a cooling circuit of the thermal management system, and a controller configured to generate control commands configured to control one or more controllable components of the thermal management system based at least in part on the sensor outputs. The one or more sensors may include one or more phase detection sensors, such as an acoustic sensor.Type: GrantFiled: March 7, 2022Date of Patent: October 17, 2023Assignee: General Electric CompanyInventor: Arthur William Sibbach
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Patent number: 11767790Abstract: A turbofan engine is provided. The turbofan engine includes a fan comprising a plurality of fan blades; a turbomachine operably coupled to the fan for driving the fan, the turbomachine comprising a compressor section, a combustion section, and a turbine section in serial flow order and together defining a core air flowpath; a nacelle surrounding and at least partially enclosing the fan; an inlet pre-swirl feature located upstream of the plurality of fan blades, the inlet pre-swirl feature attached to or integrated into the nacelle; and a means for directing incoming objects towards an outer portion of the turbofan engine in communication with the inlet pre-swirl feature.Type: GrantFiled: August 23, 2021Date of Patent: September 26, 2023Assignee: General Electric CompanyInventors: Arthur William Sibbach, Brandon Wayne Miller