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    Systems, program products, and methods for detecting thermal stability within gas turbine systems
    1.
    发明授权
    Systems, program products, and methods for detecting thermal stability within gas turbine systems 有权

    公开(公告)号：US11585234B2

    公开(公告)日：2023-02-21

    申请号：US16809134

    申请日：2020-03-04

    Applicant: General Electric Company

    Inventor： Veerappan Muthaiah ,  Timothy Andrew Healy ,  Randy Scott Rosson ,  Harold Lamar Jordan, Jr. ,  Kowshik Narayanaswamy

    IPC: F01D21/00 ,  G05B23/02

    Abstract: Systems, program products, and methods for detecting thermal stability within gas turbine systems are disclosed. The systems may include a computing device(s) in communication with a gas turbine system, and a plurality of sensors positioned within or adjacent the gas turbine system. The sensor(s) may measure operational characteristics of the gas turbine system. The computing device(s) may be configured to detect thermal stability within the gas turbine system by performing processes including calculating a lag output for each of the plurality of measured operational characteristics. The calculated lag output may be based on a difference between a calculated lag for the measured operational characteristics and the measured operational characteristic itself. The calculated lag output may be also be based on a time constant for the measured operational characteristics. The computing device(s) may also determine when each of the calculated lag outputs are below a predetermined threshold.

    SYSTEMS, PROGRAM PRODUCTS, AND METHODS FOR DETECTING THERMAL STABILITY WITHIN GAS TURBINE SYSTEMS
    2.
    发明申请
    SYSTEMS, PROGRAM PRODUCTS, AND METHODS FOR DETECTING THERMAL STABILITY WITHIN GAS TURBINE SYSTEMS 有权

    公开(公告)号：US20210277794A1

    公开(公告)日：2021-09-09

    申请号：US16809134

    申请日：2020-03-04

    Applicant: General Electric Company

    Inventor： Veerappan Muthaiah ,  Timothy Andrew Healy ,  Randy Scott Rosson ,  Harold Lamar Jordan, JR. ,  Kowshik Narayanaswamy

    IPC: F01D21/00

    Abstract: Systems, program products, and methods for detecting thermal stability within gas turbine systems are disclosed. The systems may include a computing device(s) in communication with a gas turbine system, and a plurality of sensors positioned within or adjacent the gas turbine system. The sensor(s) may measure operational characteristics of the gas turbine system. The computing device(s) may be configured to detect thermal stability within the gas turbine system by performing processes including calculating a lag output for each of the plurality of measured operational characteristics. The calculated lag output may be based on a difference between a calculated lag for the measured operational characteristics and the measured operational characteristic itself. The calculated lag output may be also be based on a time constant for the measured operational characteristics. The computing device(s) may also determine when each of the calculated lag outputs are below a predetermined threshold.

    Systems and methods for use in adapting the operation of a gas turbine
    4.
    发明授权
    Systems and methods for use in adapting the operation of a gas turbine 有权
    用于适应燃气轮机运行的系统和方法

    公开(公告)号：US09459671B2

    公开(公告)日：2016-10-04

    申请号：US13776088

    申请日：2013-02-25

    Applicant: General Electric Company

    Inventor： Randy Scott Rosson

    IPC: G06F1/26 ,  F02C9/00

    CPC classification number: G06F1/26 ,  F02C9/00

    Abstract: A control system for use in adapting the operation of a gas turbine is provided. The control system is configured to be coupled to at least one component of the gas turbine. The gas turbine is coupled to a power grid having a standardized frequency. The control system includes a processor and a memory coupled to the processor. The memory includes processor-executable instructions that, when executed by the processor, cause the control system to store a status of the at least one component of the gas turbine and generate and store a first operating setting for the at least one component. The first operating setting corresponds to a first frequency of the power grid that is less than the standardized frequency.

    Abstract translation: 提供了一种用于适应燃气轮机操作的控制系统。 控制系统被配置为联接到燃气轮机的至少一个部件。 燃气轮机连接到具有标准化频率的电网。 控制系统包括处理器和耦合到处理器的存储器。 所述存储器包括处理器可执行指令，当所述处理器执行时，所述指令使所述控制系统存储所述燃气轮机的所述至少一个部件的状态并生成并存储所述至少一个部件的第一操作设置。 第一操作设置对应于小于标准化频率的电网的第一频率。

    SYSTEMS AND METHODS FOR USE IN ADAPTING THE OPERATION OF A GAS TURBINE
    5.
    发明申请
    SYSTEMS AND METHODS FOR USE IN ADAPTING THE OPERATION OF A GAS TURBINE 有权
    用于适应气体涡轮机运行的系统和方法

    公开(公告)号：US20140244055A1

    公开(公告)日：2014-08-28

    申请号：US13776088

    申请日：2013-02-25

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Randy Scott Rosson

    IPC: G06F1/26

    CPC classification number: G06F1/26 ,  F02C9/00

    Abstract: A control system for use in adapting the operation of a gas turbine is provided. The control system is configured to be coupled to at least one component of the gas turbine. The gas turbine is coupled to a power grid having a standardized frequency. The control system includes a processor and a memory coupled to the processor. The memory includes processor-executable instructions that, when executed by the processor, cause the control system to store a status of the at least one component of the gas turbine and generate and store a first operating setting for the at least one component. The first operating setting corresponds to a first frequency of the power grid that is less than the standardized frequency.

    Abstract translation: 提供了一种用于适应燃气轮机操作的控制系统。 控制系统被配置为联接到燃气轮机的至少一个部件。 燃气轮机连接到具有标准化频率的电网。 控制系统包括处理器和耦合到处理器的存储器。 所述存储器包括处理器可执行指令，当所述处理器执行时，所述指令使所述控制系统存储所述燃气轮机的所述至少一个部件的状态并生成并存储所述至少一个部件的第一操作设置。 第一操作设置对应于小于标准化频率的电网的第一频率。

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