Modeling and Simulation of Gas Turbine Starter and Fuel Control System

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• 英文论文题名：Modeling and Simulation of Gas Turbine Starter and Fuel Control System
• 论文作者：Song Ma ; Jianguo Tan ; Yongqian Ning ; Zichang Gao
• 英文论文作者：Song Ma ; Jianguo Tan ; Yongqian Ning ; Zichang Gao ; College of Aerospace Science and Engineering ; National University of Defense Technology ; Shen yang Aircraft Design & Research Institute ; School of Control Science and Engineering ; Dalian University of Technology
• 年：2017
• 作者机构：College of Aerospace Science and Engineering,National University of Defense Technology;Shen yang Aircraft Design & Research Institute;School of Control Science and Engineering,Dalian University of Technology;
• 英文论文关键词：Gas turbine starter ; Fuel control system ; Mechanical hydraulic modeling ; Component-level model ; Simulation
• 会议召开时间：2017-07-26
• 会议录名称：第36届中国控制会议论文集（B）
• 英文会议录名称：Proceedings of the 36th Chinese Control Conference（B）
• 语种：英文
• 分类号：V235.1
• 学会代码：KZLL
• 会议名称：第36届中国控制会议
• 会议地点：中国辽宁大连
• 主办单位：中国自动化学会控制理论专业委员会
• 学会名称：中国自动化学会控制理论专业委员会
• 页数：6
• 文件大小：271k
• 原文格式：D
• 会议级别：全国

摘要

Gas turbine starter is an important component of aero-engine gas turbine starting system,and its performance directly affects the starting ability of aero-engine.In order to meet the requirements of starter power for different types of large engines and to provide theoretical basis for modification of starters,this paper pays attention to the performance of a gas turbine starter and its fuel control system.The structure and operating principle of the system are firstly analyzed.Based on the AMESim mechanical hydraulic simulation software,the component-level model of fuel control system is constructed.Then the model of the starter part is established according to the basic principles of gas dynamics and thermodynamics.By comparing the simulation results of the model with the experimental data,results show that the established model can meet the needs of engineering and thus provides a simulation platform for future research of gas turbine starter.
Gas turbine starter is an important component of aero-engine gas turbine starting system,and its performance directly affects the starting ability of aero-engine.In order to meet the requirements of starter power for different types of large engines and to provide theoretical basis for modification of starters,this paper pays attention to the performance of a gas turbine starter and its fuel control system.The structure and operating principle of the system are firstly analyzed.Based on the AMESim mechanical hydraulic simulation software,the component-level model of fuel control system is constructed.Then the model of the starter part is established according to the basic principles of gas dynamics and thermodynamics.By comparing the simulation results of the model with the experimental data,results show that the established model can meet the needs of engineering and thus provides a simulation platform for future research of gas turbine starter.

引文

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