Performance calculation and analysis of intercooled recuperated aero-engine
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摘要: 在常规循环双轴分排大涵道比涡扇发动机模型基础上,通过引入间冷器、回热器和间冷涵道模型,发展了间冷回热航空发动机(IRA)性能模拟方法.编写了相应的性能计算程序,计算并分析了一种间冷涵道独立排气的IRA的高度速度特性和节流特性.计算表明:全包线内,回热器一直可以正常换热,IRA可以正常工作.不同工况下,IRA的净推力都接近或大于对照常规循环涡扇发动机,而耗油率较对照常规循环涡扇发动机降低9%~20%.Abstract: In combination with intercooler, recuperator and intercooler duct model, an intercooled recuperated aero-engine(IRA) performance simulation methodology was developed based on conventional cycle two-spool unmixed flow high bypass ratio turbofan engine model. And an IRA performance calculation program was compiled. The characteristics of the IRA with separate intercooler duct exhaust were calculated and analyzed for the altitude velocity and throttling. The results indicate that, heat exchange process of the recuperator can always take place and IRA can operate normally in the flight envelope. In different conditions, the net thrust of the IRA is close to or higher than that of the conventional turbofan engine, while the specific fuel consumption of the IRA is reduced by 9% to 20%.
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Key words:
- intercooled /
- recuperated /
- aero-engine /
- performance simulation /
- engine characteristic
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[1] McDonald C F,Massardo A F,Rodgers C,et al.Recuperated gas turbine aeroengines:Part Ⅰ early development activities[J].Aircraft Engineering and Aerospace Technology,2008,8(2):139-157. [2] McDonald C F,Massardo A F,Rodgers C,et al.Recuperated gas turbine aeroengines:Part Ⅱ engine design studies following early development testing[J].Aircraft Engineering and Aerospace Technology,2008,8(3):280-294. [3] 张忠文,曲文浩,郑培英,等.间冷回热燃气轮机发展现状[J].航空发动机,2010,36(3):42-44. ZHANG Zhongwen,QU Wenhao,ZHENG Peiying,et al.The development state of intercooled recuperated gas turbine[J].Aeroengine,2010,36(3):42-44.(in Chinese) [4] McCarthy L S,Scott M L.The WR-21 intercooled recuperated gas turbine engine-operation and integration into royal navy type 45 destroyer power system.ASME Paper GT-2002-30266,2002. [5] Wilfert G,Sieber J,Rolt A,et al.New environmental friendly aero engine core concepts.ISABE-2007-1120,2007. [6] Rolt A M,Kyprianidis K G.Assessment of new aeroen-gine core concepts and technologies in the EU framework 6 NEWAC programme.Nice,France:27th International Congress of the Aeronautical Sciences,2010. [7] Boggia S,Rud K.Intercooled recuperated aero engine.Munchen,Germany:MTU Aero Engines,2004. [8] McDonald C F,Massardo A F,Rodgers C,et al.Recuperated gas turbine aeroengines:Part Ⅲ engine concepts for reduced emissions,lower fuel consumption,and noise abatement[J].Aircraft Engineering and Aerospace Technology,2008,8(4):408-426. [9] Gmelin T C,Hüttig G,Lehmann O.Summarized description of aircraft efficiency potentials taking account of current engine technology and foreseeable medium-term developments.Berlin,Germany:German Federal Ministry for the Environment,Nature Conservation and Nuclear Safety,FKZ UM 0706 602/01,2008. [10] Dewanji D,Rao A G,Buijtenen J P.Conceptual study of future aero-engine concepts[J].International Journal of Turbo and Jet Engines,2009,26(4):263-276. [11] Andriani R,Gamma F,Ghezzi1 U.Numerical analysis of intercooled and recuperated turbofan engine[J].International Journal of Turbo and Jet-Engines,2011,28(2):139-146. [12] Kyprianidis K G,Grnstedt T,Ogaji S O T,et al.Assessment of future aero-engine designs with intercooled and intercooled recuperated cores[J].Journal of Engineering for Gas Turbines and Power,2011,133(1):011701.1-011701.10. [13] Xu L,Kyprianidis K G,Grnstedt T.Optimization study of an intercooled recuperated aero-engine[J].Journal of Propulsion and Power,2013,29(2):424-432. [14] 曹梦源,唐海龙,陈敏.中冷回热航空涡扇发动机热力循环初步分析[J].航空动力学报,2009,24(11):2465-2470. CAO Mengyuan,TANG Hailong,CHEN Min.Preliminary analysis of thermodynamic cycle of an intercooled recuperated turbofan engine[J].Journal of Aerospace Power,2009,24(11):2465-2470.(in Chinese) [15] SONG Xingchao,TANG Hailong,CHEN Min.Throttling performance analysis of intercooled recuperated turbofan aero-engine//Proceedings of 4th International Symposium on Jet Propulsion and Power Engineering.Xi'an:,2012:564-569. [16] 龚昊,王占学,刘增文.间冷回热循环航空发动机参数匹配研究[J].航空动力学报,2012,27(8):1809-1814. GONG Hao,WANG Zhanxue,LIU Zengwen.Study on thermodynamic cycle parameter matching for intercooled recuperated aero-engine[J].Journal of Aerospace Power,2012,27(8):1809-1814.(in Chinese) [17] Sellers J F,Daniele C J.DYNGEN:a program for calculating steady-state and transient performance of turbojet and turbofan engines.NASA TND-7901,1975. [18] Walsh P P,Fletcher P.Gas turbine performance[M].2nd ed.Oxford:Blackwell Science Ltd.,2004. [19] 余建祖.换热器原理与设计[M].北京:北京航空航天大学出版社,2006.
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