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121.发明授权公开(公告)号：US12247517B2
公开(公告)日：2025-03-11
申请号：US17991781
申请日：2022-11-21
Applicant: General Electric Company
Inventor： Juergen Gerhard Hoffmann , Harold Lamar Jordan , Thomas John Freeman
Abstract: A system includes a gas turbine system having a compressor, a combustor, and a turbine. The system further includes a power management system configured to supply an injection fluid into a host fluid of the gas turbine system to manage power production of the gas turbine system, wherein the injection fluid comprises a gas mixture comprising oxygen. The system further includes a model-based controller configured to control operation of the gas turbine system, wherein the model-based controller has one or more models including consideration of the injection fluid supplied by the power management system into the host fluid.
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公开(公告)号：US20250076135A1
公开(公告)日：2025-03-06
申请号：US18953254
申请日：2024-11-20
Applicant: General Electric Company
Inventor： Robert James MacDonald , Yizhen Lin , Nicholas G. Yost , David Richard Esler
Abstract: An apparatus includes a first acoustic sensing resonator formed from a silicon substrate and has a first microelectromechanical system. The apparatus also includes a second acoustic sensing resonator formed from the silicon substrate and has a second microelectromechanical system. The second acoustic sensing resonator is arranged on the silicon substrate at a ninety degree (90°) angle with respect to the first acoustic sensing resonator and together the first acoustic sensing resonator and second acoustic sensing resonator form a torque sensor. A high temperature bonding surface is connected to the torque sensor for directly connecting the torque sensor to a metal object.
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公开(公告)号：US20250075627A1
公开(公告)日：2025-03-06
申请号：US18461088
申请日：2023-09-05
Applicant: General Electric Company
Inventor： Donald Ira Goepper , Timothy Leo Schelfaut , Taehong Kim
IPC: F01D11/22
Abstract: A method of operating a gas turbine engine is provided. The method includes receiving sensor data from one or more sensors. The method further includes receiving additional data associated with an engine event. The method further includes generating a current clearance based on at least one of the sensor data and the additional data associated with the engine event. The method further includes generating a target clearance based on at least one of the sensor data and the additional data associated with the engine event and comparing the target clearance to the current clearance. The method further includes causing the clearance adjustment system to adjust the clearance based on the comparison between the target clearance and the actual clearance by actuating the piezoelectric actuator.
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公开(公告)号：US20250074620A1
公开(公告)日：2025-03-06
申请号：US18461651
申请日：2023-09-06
Applicant: General Electric Company
Inventor： Brandon W. Miller , Daniel A. Niergarth , Arthur W. Sibbach
Abstract: An aircraft gas turbine includes a combustor that combusts compressed air and at least one fuel flow from at least one fuel source to generate combustion gases. A fuel supply system is arranged to provide at least one of a first flow of fuel to the combustor via a first fuel supply line and a second flow of a heated fuel to the combustor via a second fuel supply line. A fuel heat exchanger is arranged within the fuel supply system to generate the heated fuel that is heated above an autoignition temperature of the fuel, and a heat source communicates with the fuel heat exchanger for generating the heated fuel.
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公开(公告)号：US12244204B2
公开(公告)日：2025-03-04
申请号：US18316048
申请日：2023-05-11
Applicant: General Electric Company
Inventor： Lokaditya Ryali , Bugra H Ertas , Adam Joseph Wangler
IPC: H02K49/10 , F04D13/02 , F04D15/00 , F04D29/043
Abstract: Methods, apparatus, systems, and articles of manufacture are disclosed to a flux-modulated permanent magnet clutch. Disclosed is a magnetic clutch apparatus comprising a tension spring, an outer ring coupled to the tension spring, the outer ring including a first plurality of magnets, an inner ring coupled to an output shaft, the inner ring including a second plurality of magnets, the outer ring to magnetically engage with the inner ring, and an intermediate ring coupled to an input shaft, the intermediate ring disposed between the inner ring and the outer ring, the intermediate ring including a ferrous metal.
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Patent Agency Ranking
公开(公告)号：US12241628B2
公开(公告)日：2025-03-04
申请号：US18460078
申请日：2023-09-01
Applicant: General Electric Company
Inventor： Gurunath Gandikota , Karthikeyan Sampath , Perumallu Vukanti , Allen M. Danis , Scott M. Bush , Steven Clayton Vise , Hari Ravi Chandra , Rimple Rangrej , Saket Singh , Pradeep Naik , Neeraj Kumar Mishra , Arvind Kumar Rao , Balasubramaniam Venkatanarayanan , Ranjeet Kumar Mishra
Abstract: A swirler assembly for a combustor includes at least one swirler including a plurality of swirl vanes arrayed about an axis of the swirler. The plurality of swirl vanes includes a first ring of first sub-vanes and a second ring of second sub-vanes, the first ring of first sub-vanes and the second ring of second sub-vanes being separated by a gap therebetween.
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127.发明授权公开(公告)号：US12241426B2
公开(公告)日：2025-03-04
申请号：US16238777
申请日：2019-01-03
Applicant: General Electric Company
Inventor： Christopher David King , Jessie Thorup
Abstract: Provided are systems and methods of controlling load share in a multi-engine propulsion system. A load share participation value indicative of a load share participation regime for a first engine may be received and a load sharing requirement control command for the first engine may be output. The load share participation value may depend or be based at least in part on one or more operating conditions of a second engine. The load sharing requirement control command for the first engine may depend on whether the load share participation value indicates a full-participation load share regime for the first engine, a partial-participation load share regime for the first engine, or a non-participation load share regime for the first engine.
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公开(公告)号：US12241382B2
公开(公告)日：2025-03-04
申请号：US17490436
申请日：2021-09-30
Applicant: General Electric Company
Inventor： Eduardo Aguilar Armendariz , Pamela M. Boehm , Kanahayya Dudhale , Shivam Mittal , William J. Simpson
Abstract: A system and method for reducing the vibration response of a rotating system are provided. In one aspect, an optimized balance shot or solution that indicates one or more physical locations at which one or more balancing weights are to be added or removed from the rotating system is generated. The balance shot is generated based on a transfer function that is customized specifically for the rotating system. The transfer function is generated by applying one or more machine-learned models to parameter values for parameters that are associated with the rotating system. The machine-learned models can generate main effects plots, and from the plots, an effective set of parameter values can be determined. The transfer function can be generated using the effective set of parameter values so that the transfer function used to generate the balance shot is optimized specifically for the rotating system undergoing the balancing process.
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公开(公告)号：US20250070831A1
公开(公告)日：2025-02-27
申请号：US18722125
申请日：2022-12-20
Applicant: General Electric Company
Inventor： Stephen F. BUSH
IPC: H04B7/0456 , H04B7/0417 , H04L5/00
Abstract: A radio network (e.g., a multiple-input multiple-output (MIMO) radio network) includes a transmitter node and a receiver node. The transmitter node is configured to determine whether a radio link (e.g., a MIMO link) associated with a plurality of subchannels is carrying time sensitive networking (TSN) traffic. In accordance with a determination that the radio link is carrying TSN traffic, the transmitter node is configured to obtain configuration values (e.g., a plurality of channel path coefficients) based on estimated quality of each of the plurality of subchannels; adjust the configuration values such that variance in quality of the plurality of subchannels is minimized; and transmit data to the receiver node via the plurality of subchannels in accordance with the adjusted configuration values.
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公开(公告)号：US20250067435A1
公开(公告)日：2025-02-27
申请号：US18943011
申请日：2024-11-11
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Manampathy G. Giridharan , Pradeep Naik , Michael A. Benjamin
Abstract: A combustor having a casing, an inner liner, an outer liner, a compressed air passageway, a combustion chamber and a set of dilution passages. The compressed air passageway being formed between the casing, the inner liner and the outer liner. The combustion chamber being at least partially defined by the inner liner and the outer liner. The set of dilution passages extending through at least one of the inner liner or the outer liner. Each dilution passage of the set of dilution passages extending between an inlet fluidly coupled to the compressed air passageway and a dilution hole fluidly coupled to the combustion chamber.
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