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Modeling method and equipment for predicting output data of gas turbine in starting process

A start-up process, gas turbine technology, applied in nuclear methods, electrical digital data processing, computer-aided design, etc., can solve the problems of low model accuracy and low versatility

Pending Publication Date: 2020-11-20
新奥能源动力科技(上海)有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The invention provides a modeling method and equipment for predicting the output data of the gas turbine start-up process, which are used to solve the problems of low model accuracy and low versatility existing in the existing modeling methods for predicting the output data of the gas turbine start-up process

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  • Modeling method and equipment for predicting output data of gas turbine in starting process
  • Modeling method and equipment for predicting output data of gas turbine in starting process
  • Modeling method and equipment for predicting output data of gas turbine in starting process

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Embodiment 1

[0103] The embodiment of the present invention provides a modeling method for predicting the output data of the start-up process of the gas turbine, which is applied to the identification and modeling scene of the start-up process of the micro-gas turbine, such as figure 1 As shown, the method includes:

[0104] Step S101, performing parameter collection during multiple start-ups of the gas turbine, and correspondingly obtaining a plurality of training samples;

[0105] The embodiment of the present invention conducts identification modeling based on the operating data of the start-up process of the micro-gas turbine, uses the parameters collected from the start-up process of the micro-gas turbine as training samples, performs identification modeling and model training, and obtains an output prediction model, which will be described in detail below.

[0106] During multiple start-ups of the gas turbine, at least one type of parameter whose coupling degree does not exceed a set...

Embodiment 2

[0154] In this embodiment, a micro gas turbine with a stand-alone power range of 30KW-1MW is taken as an example for illustration.

[0155] When establishing the output data prediction model of the gas turbine start-up process in this embodiment, first obtain the training samples, select multiple sets of start-up process data of the above-mentioned micro gas turbine, take the time interval of 0.5s as the sampling point, and select the gas turbine start-up process according to the characteristics of the gas turbine. Smallest set of variables. Extract 33 groups of minimum variable group data in the start-up process of micro gas turbines operating at different ambient temperatures, that is, the input data. Among them, 32 groups of gas turbine start-up process data are used as training samples, and 1 group of gas turbine start-up process data is used as test samples. Each group of samples contains 1322 For the data, in this embodiment, it is required that the error of the dynamic ...

example 1

[0172] Using the SVM optimization modeling method, only using the SVM algorithm, the ambient temperature, compressor inlet pressure, natural gas flow and starting current are used as the input data of the model, and the gas turbine speed and exhaust temperature are used as the output data of the model for model training.

[0173] refer to Figure 13 , is the prediction result graph of the SVM-optimized gas turbine speed provided by the embodiment of the present invention;

[0174] refer to Figure 14 , is a graph of the prediction results of the exhaust gas temperature optimized by the SVM provided by the embodiment of the present invention.

[0175] When this embodiment only uses the SVM algorithm to perform model training on the above data, the results of the model-predicted gas turbine speed and exhaust temperature are as follows: Figure 13 , Figure 14 As shown, according to the calculation of the prediction results, it can be known that the mean square error of the ga...

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Abstract

The invention provides a modeling method and equipment for predicting output data of a gas turbine in a starting process, and the method comprises the steps: carrying out the parameter collection in aplurality of starting processes of the gas turbine, and correspondingly obtaining a plurality of training samples; taking part of data in the training sample as input data of a network model; and analyzing control parameters of an input data prediction support vector machine (SVM) algorithm by utilizing a grey wolf optimization (GWO) algorithm, and adjusting model parameters of the network modelby taking the other part of data in the output training sample as a target according to the input data under the control of the control parameters by utilizing the SVM algorithm to obtain an output prediction model. According to the modeling method and device for predicting the output data of the gas turbine in the starting process, the problems that an existing modeling method for predicting theoutput data of the gas turbine in the starting process is low in model precision and universality are solved.

Description

technical field [0001] The invention relates to the technical field of gas turbines, in particular to a modeling method and equipment for predicting the output data of the gas turbine start-up process. Background technique [0002] The gas turbine is one of the core components of the gas-steam combined cycle, which has the advantages of high efficiency, fast start-up, and low environmental pollution. Gas turbine start-up refers to the process in which the gas turbine reaches a certain speed from a stationary (cranking) state. In the study of gas turbine start-up characteristics, the method of establishing a mathematical simulation model for performance evaluation is generally adopted, and the actual operation process of the gas turbine is simulated by establishing a model, and performance analysis and prediction are performed, so as to obtain the control law, control the operation of the gas turbine, and ensure the gas turbine operation. efficient and stable operation. [...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/27G06F30/28G06N20/10G06F113/08G06F119/08G06F119/14
CPCG06F30/27G06F30/28G06N20/10G06F2113/08G06F2119/14G06F2119/08
Inventor 张孟然张琪鲍其雷刘青山刘德玉毕辉阮健斌
Owner 新奥能源动力科技(上海)有限公司
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