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公开(公告)号：US10697318B2
公开(公告)日：2020-06-30
申请号：US15404903
申请日：2017-01-12
Applicant: General Electric Company
Abstract: A non-transitory computer readable medium stores instructions that are executed by a processor of a monitoring that when executed, the processor receives a state of at least one operational parameter of the turbomachinery. Then, the processor determines whether the state is within a region of accuracy of a stored record of a stored state stored in the memory. When the state is within the region of accuracy, the processor determines at least one operating condition from the stored record. Alternatively, when the state is not within the first region of accuracy, the processor stores the state as a new record in the memory.
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公开(公告)号：US20180187574A1
公开(公告)日：2018-07-05
申请号：US15450899
申请日：2017-03-06
Applicant: General Electric Company
Inventor： Prabhanjana Kalya , Pramod Kumar Yadav , Sidharth Abrol , Giriprasad Chebiyyam
CPC classification number: F01K23/101 , F01K13/02 , F02C7/00 , F05D2260/80 , H02K7/1823 , Y02E20/16
Abstract: A monitoring system of a combined cycle power plant having a topping cycle performed by a gas turbine and a bottoming cycle performed by a steam turbine, the monitoring system. The monitoring system includes a processor that receives a first set of data indicating a first measurement value of an operating parameter of the combined cycle power plant. The processor determines a baseline efficiency of the process based on the first measurement value using a bottoming cycle performance (BCP) model. The processor determines a threshold based on the baseline efficiency. The processor receives a second set of data indicating a second measurement value of the operating parameter. The processor compare the threshold to an operational efficiency based on the second measurement value using the BCP model, and provides an indication of a decrease in efficiency of the process if the operational efficiency is below the threshold.
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公开(公告)号：US20190032510A1
公开(公告)日：2019-01-31
申请号：US16077138
申请日：2017-02-01
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Sidharth Abrol , Sangeeta Balram , Prem Kumar Patchaikani , Prabhanjana Kalya
Abstract: A method for predicting an anomaly in a combustor (16) is presented. The method includes receiving signals representative of parameters in one or more combustion cans (22, 24) of the combustor, generating a plurality of patterns based on a permutation entropy window and the signals, identifying a plurality of pattern categories in the plurality of patterns, determining a permutation entropy based on the plurality of patterns and the plurality of pattern categories, and predicting an anomaly in the combustor based on the permutation entropy. The method further includes comparing the plurality of pattern categories to determined permutations of pattern categories if the anomaly is present in the combustor, and predicting a category of the anomaly based on the comparison of the plurality of pattern categories to the determined permutations of pattern categories.
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4.发明申请MODEL-BASED FEED FORWARD APPROACH TO COORDINATED AIR-FUEL CONTROL ON A GAS TURBINE 有权基于模型的进料方法对气体涡轮机协调的空气燃料控制公开(公告)号：US20150240726A1
公开(公告)日：2015-08-27
申请号：US14190181
申请日：2014-02-26
Applicant: General Electric Company
Inventor： Jonathan York Smith , John Rogers Huey , Prabhanjana Kalya
IPC: F02C9/22
CPC classification number: F02C9/22 , F02C9/00 , F05D2260/821 , F05D2270/05 , F05D2270/71 , G05B13/042
Abstract: Presented herein are turbine machines, turbine control systems, methods, and computer-readable storage devices for controlling turbines including a compressor, a combustion system, and a turbine section comprising a turbine operating at an initial turbine output while using initial parameter values for the respective control parameters of the turbine. The techniques involve, for respective selected control parameters, selecting an adjustment of the initial parameter value of the selected control parameter, and predicting a predicted turbine output of the turbine operated using the adjustment of the selected control parameter and the initial parameter values for other control parameters; comparing the predicted turbine outputs for the adjustments of the respective control parameters to select, from the control parameters, a target control parameter having a target adjustment that results in the target turbine output; and operating the turbine with the target adjustment of the target control parameter.
Abstract translation: 这里提出的是用于控制涡轮机的涡轮机，涡轮机控制系统，方法和计算机可读存储装置，包括压缩机，燃烧系统和涡轮机部分，其包括在初始涡轮机输出处操作的涡轮机，同时使用相应的初始参数值 涡轮机的控制参数。 这些技术涉及对于各个所选择的控制参数，选择所选择的控制参数的初始参数值的调整，并且使用所选择的控制参数的调整和用于其他控制的初始参数值来预测所操作的涡轮机的预测涡轮机输出 参数; 比较预测的涡轮机输出用于各个控制参数的调整，从控制参数中选择具有导致目标涡轮机输出的目标调节的目标控制参数; 并且利用目标控制参数的目标调整来操作涡轮机。
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公开(公告)号：US10704427B2
公开(公告)日：2020-07-07
申请号：US15450899
申请日：2017-03-06
Applicant: General Electric Company
Inventor： Prabhanjana Kalya , Pramod Kumar Yadav , Sidharth Abrol , Giriprasad Chebiyyam
Abstract: A monitoring system of a combined cycle power plant having a topping cycle performed by a gas turbine and a bottoming cycle performed by a steam turbine, the monitoring system. The monitoring system includes a processor that receives a first set of data indicating a first measurement value of an operating parameter of the combined cycle power plant. The processor determines a baseline efficiency of the process based on the first measurement value using a bottoming cycle performance (BCP) model. The processor determines a threshold based on the baseline efficiency. The processor receives a second set of data indicating a second measurement value of the operating parameter. The processor compare the threshold to an operational efficiency based on the second measurement value using the BCP model, and provides an indication of a decrease in efficiency of the process if the operational efficiency is below the threshold.
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Patent Agency Ranking
公开(公告)号：US20180298817A1
公开(公告)日：2018-10-18
申请号：US15485944
申请日：2017-04-12
Applicant: General Electric Company
Inventor： Prabhanjana Kalya , Sidharth Abrol , Matthew John McKeever , David Spencer Ewens
CPC classification number: F02C7/047 , F01D25/02 , F01D25/10 , F02C9/18 , F04D27/001 , F04D27/009 , F04D27/0292 , F05D2220/32 , F05D2260/81 , F05D2260/83 , Y02T50/675
Abstract: A system includes a controller coupled to an inlet bleed heat system of a compressor. The controller is configured to detect an icing condition of an inlet portion of the compressor by determining a current compressor efficiency value of the compressor, a current compressor flow value of the compressor, or any combination thereof, comparing the current compressor efficiency value to a compressor efficiency model of the compressor, the current compressor flow value to a compressor flow model of the compressor, or any combination thereof, and providing an icing indication to the inlet bleed heat system if a first difference between the current compressor efficiency value and the compressor efficiency model is greater than a first threshold, a second difference between the current compressor flow value and the compressor flow model is greater than a second threshold, or any combination thereof.
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公开(公告)号：US20180016992A1
公开(公告)日：2018-01-18
申请号：US15208263
申请日：2016-07-12
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Prabhanjana Kalya , Abhijit Kulkarni , Vikas Handa , Pradeep Kumar Vavilala , Vamshi Kandula
IPC: F02C9/54
CPC classification number: F02C9/28 , F05B2270/20 , F05B2270/504 , F05B2270/709 , F05D2270/44
Abstract: A system includes a processor configured to execute an artificial neural network (ANN). The processor is configured to receive one or more operational parameters associated with an operation of a turbine system. The turbine system includes one or more combustors. The processor is further configured to analyze, via the ANN, the one or more operational parameters to determine a characteristic pattern, and to generate, via the ANN, an output based at least in part on the determined characteristic pattern. The output includes an indication of an intensity of a flame of the one or more combustors to determine a presence or an absence of the flame.
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公开(公告)号：US09639071B2
公开(公告)日：2017-05-02
申请号：US14149349
申请日：2014-01-07
Applicant: General Electric Company
Inventor： Prabhanjana Kalya , Steven William Backman , Laura Lea Boes , David Spencer Ewens , Trevor Valder Jones
CPC classification number: G05B15/00 , F02C7/228 , F02C9/00 , F02C9/28 , F02C9/34 , F05D2270/08 , F05D2270/082 , F23N2037/02 , F23N2041/20 , F23R3/34
Abstract: A method and system for transferring between combustion modes in a gas turbine engine is provided. A processor generates data representative of an initial set of splits for providing at least one of fuel and air to at least one combustor in the gas turbine engine. A gas turbine engine model module generates data representative of at least one engine operating condition. A first split calculation module generates data representative of at least one set of active control splits to control the engine in a first combustion mode, using as an input the initial split data. A second split calculation module generates data representative of at least one set of passive control splits to control the engine in at least a second combustion mode. Transfer between combustion modes may be accomplished via use of at least one of the active control splits and the passive control splits.
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公开(公告)号：US10662959B2
公开(公告)日：2020-05-26
申请号：US15473776
申请日：2017-03-30
Applicant: General Electric Company
Inventor： Sidharth Abrol , Karl Dean Minto , Nisam Palakkavalappil Rahiman , Prabhanjana Kalya , Wrichik Basu , Corey Nicholas Bufi
Abstract: A non-transitory computer-readable storage medium storing one or more processor-executable instructions wherein the one or more instructions, when executed by a processor of a controller, cause acts to be performed including receiving signals representative of pressure between respective compressor blade tips and a casing of a compressor at one or more stages, generating multiple patterns based on a permutation entropy window and the signals, identifying multiple pattern categories in the multiple patterns, determining a permutation entropy based on the multiple patterns and the multiple pattern categories, predicting an anomaly in the compressor based on the permutation entropy, comparing the multiple pattern categories to determined permutations of pattern categories when an anomaly is present in the compressor, and predicting a category of the anomaly based on the comparison of the multiple pattern categories to the determined permutation of pattern categories.
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公开(公告)号：US10508597B2
公开(公告)日：2019-12-17
申请号：US15485944
申请日：2017-04-12
Applicant: General Electric Company
Inventor： Prabhanjana Kalya , Sidharth Abrol , Matthew John McKeever , David Spencer Ewens
Abstract: A system includes a controller coupled to an inlet bleed heat system of a compressor. The controller is configured to detect an icing condition of an inlet portion of the compressor by determining a current compressor efficiency value of the compressor, a current compressor flow value of the compressor, or any combination thereof, comparing the current compressor efficiency value to a compressor efficiency model of the compressor, the current compressor flow value to a compressor flow model of the compressor, or any combination thereof, and providing an icing indication to the inlet bleed heat system if a first difference between the current compressor efficiency value and the compressor efficiency model is greater than a first threshold, a second difference between the current compressor flow value and the compressor flow model is greater than a second threshold, or any combination thereof.
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