标题: 合成气与燃油共烧之微涡轮发电系统之性能实验分析与控制系统设计
Experimental Analyses of Engine Performance and the Design of Control System on Micro Gas Turbine Engine Using the Mixture of Syn-Gas and Liquid Fuel
作者: 陈俊勋
CHEN CHIUN-HSUN
国立交通大学机械工程学系(所)
关键字: 低热值燃料;合成气;微型气涡轮引擎;实验性能分析;Low-heating value fuel;Mixture of heavy-oil and synthesis-gas;micro gasturbine engine;experimental analysis of engine performance
公开日期: 2008
摘要: 因应二氧化碳减量与石油匮乏问题,并如何利用台湾蕴藏之再生能源及适时发展新
能源是目前能源发展之政策。本计画是一延续性计画,在上一年度(95.12~96.12),以
低热值之合成气与燃油预混做为燃料,以一已开发完成的燃油气涡轮引擎作为数值模拟
的对象,将所获得的成果,应用在本年度实验计画,根据其预测将以燃油为燃料的燃烧
室重新改装成为适合低热值气体燃料之微涡轮引擎燃烧系统,然后再根据此燃烧动力系
统之性能来进行后段发电系统的设计与建立。本年度研究主要内容包括此微涡轮引擎的
可行性评估、燃烧室设计、零组件测试以及引擎运转。最后提出合成气与燃油混合共烧
涡轮引擎的操作程序与规范,以作为未来整合分散式发电系统的依据,使能源作更有效
的利用。
The utilization of renewable energy and development of new energy sources are the
present governmental energy policy to encounter the more and more stringent shortage of
fossil fuels and environmental regulations for carbon dioxide reduction in the new century.
This proposal is an extensional one. In the last awarded project, it has completely the
simulation and evaluation of a combustor of a micro-turbine by using the low-heating value
synthesis gas to mix with the heavy oil as the fuel. This proposal, according to the predicted
results of the last project, intends to analyze the engine performance of the micro gas turbine
engine experimentally when such low-heating value fuel is applied. The combustion
chamber of a micro gas turbine will be re-designed by modifying the burner from a liquid-fuel
burning system into a gas burning one to generate the combustion power. Then, the
corresponding sensors and actuators for the micro gas turbine system will also be established.
The measurement data which indicate the engine performance will be analysis and evaluate
for the extending generator system. As the design procedure of engine is finished, the
fabrication, component tests, and operation of the developed gas turbine engine system are
then performed for parametric analysis to establish the start-up and operation procedure.
The aforementioned design procedure can be used as a model in the future design of micro
gas turbine engine for power generation.
官方说明文件#: NSC97-2623-7009-006-ET
URI: http://hdl.handle.net/11536/102644
https://www.grb.gov.tw/search/planDetail?id=1620072&docId=277142
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