電站用燃?xì)廨啓C(jī)建模及控制系統(tǒng)分析與仿真
[Abstract]:In addition to the variable operating performance of the gas turbine system, the performance of the gas turbine control system also determines the economic and safety performance of the whole system. In order to ensure the safe and reliable operation of the gas turbine system, it is necessary not only to improve the performance of the gas turbine itself, but also to design a more reliable and effective control system. It is precisely because the gas turbine control system plays a very important role that several famous foreign gas turbine manufacturing companies have launched the gas turbine control system for power stations with their own property rights. The more common include GE SPEEDTRONICTMMark control system, Siemens developed TELEPER XP/3000 control system and so on. At present, most of the domestic gas turbine power stations are directly imported into foreign control systems, and foreign companies have listed the control technology as one of the core technologies that can not be transferred. With the deepening of gas turbine technology research in China and the urgent requirements of gas turbine localization, it is imperative to develop gas turbine control system with our own intellectual property rights. In this paper, a single-shaft gas turbine for a power station is taken as the research object. The simulation model of the full working condition performance of the gas turbine for power station is established. The steady-state operation results of the model are in good agreement with the experimental data, and the accuracy of the model is verified. The control system of gas turbine for power station is also analyzed in this paper. The control logic algorithm of each sub-module in the control system is analyzed in detail, and the simplified controller design is carried out. On this basis, the simulation models of gas turbine and its control system are built on Matlab/Simulink simulation platform, and the dynamic performance simulation test of the system is carried out. The simulation results are in accordance with the actual operation law of gas turbine, which proves the rationality and availability of the model. At the same time, through the analysis of the simulation results, it is proved that the gas turbine controller designed in this paper can meet the requirements of gas turbine control and can be used as the basis of further research and development.
【學(xué)位授予單位】:上海交通大學(xué)
【學(xué)位級別】:碩士
【學(xué)位授予年份】:2014
【分類號】:TM62
【參考文獻(xiàn)】
相關(guān)期刊論文 前10條
1 李麟章;;大型單軸燃?xì)?蒸汽聯(lián)合循環(huán)機(jī)組控制系統(tǒng)及其特點[J];電力系統(tǒng)自動化;2006年18期
2 高建強(qiáng);張穎;陳鴻偉;李瓊;;燃?xì)廨啓C(jī)排氣溫度對聯(lián)合循環(huán)熱經(jīng)濟(jì)性的影響[J];動力工程學(xué)報;2011年04期
3 潘蕾,楊瑜文,林中達(dá);大型單軸燃?xì)廨啺l(fā)電機(jī)組主控制系統(tǒng)功率調(diào)節(jié)的設(shè)計策略[J];發(fā)電設(shè)備;2003年06期
4 黃開明,周劍波,劉杰,黃金泉,成本林;渦軸發(fā)動機(jī)起動過程的一種氣動熱力學(xué)實時模型[J];航空動力學(xué)報;2004年05期
5 任志彬;孟光;王廷興;Jay Fletch;;基于Modelica和Dymola的航空發(fā)動機(jī)燃?xì)獍l(fā)生器的建模與性能仿真[J];航空發(fā)動機(jī);2006年04期
6 張會生,劉永文,蘇明,翁史烈;燃?xì)廨啓C(jī)速度調(diào)節(jié)過程的仿真研究[J];計算機(jī)仿真;2002年01期
7 劉冰;彭淑宏;;某重型燃?xì)廨啓C(jī)動態(tài)建模及性能仿真研究[J];計算機(jī)仿真;2012年09期
8 曾進(jìn),任慶生,翁史烈,孫薇榮;基于神經(jīng)網(wǎng)絡(luò)的燃?xì)廨啓C(jī)動態(tài)過程仿真[J];熱能動力工程;2000年04期
9 崔凝;王兵樹;李斌;趙文升;;變幾何多級軸流壓氣機(jī)全工況性能預(yù)測模型[J];熱能動力工程;2007年05期
10 夏迪;王永泓;;PG9171E型燃?xì)廨啓C(jī)變工況計算模型的建立[J];熱能動力工程;2008年04期
本文編號:2493380
本文鏈接:http://sikaile.net/falvlunwen/zhishichanquanfa/2493380.html