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    Combustion Tuning for a Gas Turbine Power Plant Using Data-Driven and Machine Learning Approach

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 003::page 031021-1
    Author:
    Li, Suhui
    ,
    Zhu, Huaxin
    ,
    Zhu, Min
    ,
    Zhao, Gang
    ,
    Wei, Xiaofeng
    DOI: 10.1115/1.4050020
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Conventional physics-based or experimental-based approaches for gas turbine combustion tuning are time consuming and cost intensive. Recent advances in data analytics provide an alternative method. In this paper, we present a cross-disciplinary study on the combustion tuning of an F-class gas turbine that combines machine learning with physics understanding. An artificial-neural-network-based (ANN) model is developed to predict the combustion performance (outputs), including NOx emissions, combustion dynamics, combustor vibrational acceleration, and turbine exhaust temperature. The inputs of the ANN model are identified by analyzing the key operating variables that impact the combustion performance, such as the pilot and the premixed fuel flow, and the inlet guide vane angle. The ANN model is trained by field data from an F-class gas turbine power plant. The trained model is able to describe the combustion performance at an acceptable accuracy in a wide range of operating conditions. In combination with the genetic algorithm, the model is applied to optimize the combustion performance of the gas turbine. Results demonstrate that the data-driven method offers a promising alternative for combustion tuning at a low cost and fast turn-around.
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      Combustion Tuning for a Gas Turbine Power Plant Using Data-Driven and Machine Learning Approach

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4277356
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorLi, Suhui
    contributor authorZhu, Huaxin
    contributor authorZhu, Min
    contributor authorZhao, Gang
    contributor authorWei, Xiaofeng
    date accessioned2022-02-05T22:20:05Z
    date available2022-02-05T22:20:05Z
    date copyright2/24/2021 12:00:00 AM
    date issued2021
    identifier issn0742-4795
    identifier othergtp_143_03_031021.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277356
    description abstractConventional physics-based or experimental-based approaches for gas turbine combustion tuning are time consuming and cost intensive. Recent advances in data analytics provide an alternative method. In this paper, we present a cross-disciplinary study on the combustion tuning of an F-class gas turbine that combines machine learning with physics understanding. An artificial-neural-network-based (ANN) model is developed to predict the combustion performance (outputs), including NOx emissions, combustion dynamics, combustor vibrational acceleration, and turbine exhaust temperature. The inputs of the ANN model are identified by analyzing the key operating variables that impact the combustion performance, such as the pilot and the premixed fuel flow, and the inlet guide vane angle. The ANN model is trained by field data from an F-class gas turbine power plant. The trained model is able to describe the combustion performance at an acceptable accuracy in a wide range of operating conditions. In combination with the genetic algorithm, the model is applied to optimize the combustion performance of the gas turbine. Results demonstrate that the data-driven method offers a promising alternative for combustion tuning at a low cost and fast turn-around.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCombustion Tuning for a Gas Turbine Power Plant Using Data-Driven and Machine Learning Approach
    typeJournal Paper
    journal volume143
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4050020
    journal fristpage031021-1
    journal lastpage031021-7
    page7
    treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 003
    contenttypeFulltext
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