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    SYSTEMS AND METHOD FOR DISTRIBUTED ENERGY RESOURCES POWER ESTIMATION
    62.
    发明申请
    SYSTEMS AND METHOD FOR DISTRIBUTED ENERGY RESOURCES POWER ESTIMATION 有权

    公开(公告)号：US20240405565A1

    公开(公告)日：2024-12-05

    申请号：US18327594

    申请日：2023-06-01

    Applicant: General Electric Company

    Inventor： Bojun Feng ,  Nurali Virani ,  Honggang Wang ,  Benoit Christophe ,  Kiran Kumar Pratapagiri

    IPC: H02J3/38 ,  H02J3/00

    Abstract: A system for predicting performance of electric power generation and delivery systems is provided. The system includes a computing device including at least one processor in communication with at least one memory. The at least one processor is programmed to store a first plurality of attribute data for a plurality of measured assets attached to a grid, store a plurality of constraints for matching measured assets to unmeasured assets, receive a second plurality of attribute data for an unmeasured asset attached to the grid, compare the first plurality of attribute data to the second plurality of attribute data and the plurality of constraints associated with the unmeasured asset, determine a measured asset of the plurality of measured assets to assign to the unmeasured asset based on the comparison, and determine a performance forecast for the unmeasured asset based on a power performance of the determined measured asset.

    Solid oxide fuel cell assembly
    66.
    发明授权
    Solid oxide fuel cell assembly 有权

    公开(公告)号：US12074350B2

    公开(公告)日：2024-08-27

    申请号：US17581155

    申请日：2022-01-21

    Applicant: General Electric Company

    Inventor： Honggang Wang ,  Michael Anthony Benjamin ,  Seung-Hyuck Hong ,  Richard L. Hart

    IPC: H01M8/04111 ,  H01M4/86 ,  H01M8/12

    CPC classification number: H01M8/04111 ,  H01M4/8652 ,  H01M2004/8684 ,  H01M2008/1293 ,  H01M2250/20

    Abstract: A propulsion system for an aircraft, the aircraft including an aircraft fuel supply, the propulsion system including: a turbomachine including a compressor section, a combustion section, and a turbine section arranged in serial flow order, the combustion section configured to receive a flow of aviation fuel from the aircraft fuel supply; and a fuel cell assembly including a fuel cell stack having a solid oxide fuel cell, the solid oxide fuel cell defining an outlet positioned to remove output products from the solid oxide fuel cell and provide the output products to the combustion section, the solid oxide fuel cell including a cathode; an electrolyte layer; and an anode positioned opposite the electrolyte layer from the cathode, the anode including a cermet, the cermet including less than 25% by volume nickel.

    GAS TURBINE COMBUSTION SECTION HAVING AN INTEGRATED FUEL CELL ASSEMBLY
    68.
    发明公开
    GAS TURBINE COMBUSTION SECTION HAVING AN INTEGRATED FUEL CELL ASSEMBLY 审中-公开

    公开(公告)号：US20240162459A1

    公开(公告)日：2024-05-16

    申请号：US17984699

    申请日：2022-11-10

    Applicant: General Electric Company

    Inventor： Seung-Hyuck Hong ,  Richard L. Hart ,  Honggang Wang ,  Anil Raj Duggal ,  Michael Anthony Benjamin

    IPC: H01M8/04111

    CPC classification number: H01M8/04111 ,  B64D2027/026

    Abstract: 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.

    Integrated fuel cell and combustor assembly
    69.
    发明授权
    Integrated fuel cell and combustor assembly 有权

    公开(公告)号：US11978934B2

    公开(公告)日：2024-05-07

    申请号：US17406894

    申请日：2021-08-19

    Applicant: General Electric Company

    Inventor： Honggang Wang ,  Michael A. Benjamin

    IPC: H01M8/04 ,  H01M8/04701 ,  H01M8/04858 ,  H01M8/0662 ,  H01M8/24

    CPC classification number: H01M8/0662 ,  H01M8/04738 ,  H01M8/0491 ,  H01M8/24 ,  H01M2250/20

    Abstract: An integrated fuel cell and combustor assembly, and a related method. The assembly includes a combustor having a combustor geometry and a combustor exit temperature. The assembly further includes multiple fuel cells fluidly coupled to the combustor, the multiple fuel cells being configured to generate a fuel cell power output using fuel and air directed into the multiple fuel cells and to direct a fuel and air exhaust from the multiple fuel cells into the combustor. The multiple fuel cells include multiple fuel cell control groups arranged in a predetermined electrical configuration about the combustor geometry. Each of the multiple fuel cell control groups has an adjustable electrical current bias.

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