王文杰
摘要:本文参考俄罗斯新研制的一种双通道燃气轮机ΓΤУ-18ПС,它的外涵增压空气经与内涵燃机的排气换热后驱动热空气涡轮,该涡轮与内涵燃机动力涡轮共轴输出功率,可大幅提高燃气轮机的输出功率和循环效率。将这种空气底部回热复合循环方式用于某型涡扇发动机改型燃气轮机方案,经计算分析可使燃气轮机的性能和热效率明显提高。
关键词: 双涵道;燃气轮机;复合循环
Abstract: This paper gives a
discussion on the newly dual-ducted ΓΤУ-18ПС gas turbine developed in Russia.In
this turbine,the compressed air passing the engine exchanges heat with air flow
passing through the core to drive the hot air turbine.Air turbine shares the
same shaft with the power turbine to output power.In such way,the gas turbine
might output much higher power and achieve cycle efficiency greatly.This method
of air basal heat regenerative cycle is used in the plan for gas turbine
modified on the turbine engine.The calculation analysis shows that this method
may improve the turbine performance and its heat efficiency.
Keywords: Dual Bypass;Gas
Turbine;Compound Cycle
参考文献:
[1]H.Saravanamuttoo,G.Rogers
and H.Cohen.Gas TurbineTheory.5th Edition,Pearso Education Ltd.,England,2005.
[2]P.P.Walsh,P.Fletcher.Gas
Turbine Performance.2nd Edition,Thomson Press Ltd,India,2004.
[3]廉小纯,吴虎.航空燃气轮机原理.国防工业出版社,2001.
[4]王仲奇,秦仁.透平机械原理.机械工业出版社,1985.
[5]沈炳正,燃气轮机装置.机械工业出版社.1981.
[6]Lee
S,Langston.Gas Turbine Industry Overview.ASME International Gas Turbine
Institute,Global Gas Turbine News,No.2,1999.
[7]徐建中等.斯贝MK202船用改装机总体参数选择及性能计算.中国科学院工程热物理研究所,1981.
[8]徐建中等.斯贝发动机低压压气机切顶的气动热力学设计计算.中国科学院工程热物理研究所,1982.
[9]葛满初等.斯贝发动机工业及舰用改型透平部件改型方案分析及气动计算报告.中国科学院工程热物理研究所,1981.
[10]徐建中等.斯贝发动机改进的设想、方案和技术途径.430厂/中国科学院力学研究所斯贝改进联合小组,1979.
|