短周期涡轮实验的发展趋势

赵晓路; 唐菲

短周期涡轮实验的发展趋势

赵晓路,
唐菲

中国科学院工程热物理研究所, 北京 100080

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出版历程
- 收稿日期: 2006-03-27
- 修回日期: 2006-11-07
- 刊出日期: 2007-04-28

Development trend of short-duration turbine experiments

Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100080, China

摘要

摘要: 对国外短周期涡轮实验技术的发展及其应用范围开拓的情况进行了综述和分析.比较了长短周期涡轮实验技术各自的优点和不足.近年来, 在发展高性能航空发动机的需求带动下, 短周期涡轮实验技术正在努力克服自身的薄弱环节, 力争达到长周期涡轮实验技术所能达到的性能测试精度.其发展目标是争取部分替代长周期涡轮实验, 由单纯机理性实验平台向部件性能研发平台扩展.同时, 作为重要的基础研究平台, 短周期涡轮实验台在机理研究领域也有所拓宽, 开始被应用于新设计理念的验证、CFD设计分析软件的校验等新的领域.
- 航空、航天推进系统 /
- 涡轮实验技术 /
- 短周期 /
- 传热 /
- 流动机理 /
- CFD软件校验
Abstract: The development and expansion of overseas short-duration turbine testing techniques were summarized and analyzed by comparing the advantages and disadvantages of short-/long-duration turbine testing techniques. Spurred by the demand of developing high performance aeroengine, the short-duration turbine testing technique was improved greatly to achieve the measurement accuracy of long-duration turbine testing technique.The purpose of short-duration turbine testing technique is to replace partially long-duration turbine testing technique by developing from a mechanics investigation platform into a performance investigation platform. As an important basic study platform, short-duration turbine testing platform has developed in the mechanism research field and has now been applied to validation of new design concept and check of CFD software.
- aerospace propulsion system /
- turbine testing technique /
- short-duration /
- heat transfer /
- flow mechanics /
- calibration of CFD software

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参考文献(34)

[1]	Haldeman C W,Dunn M G,Abhari R S,et al.Experimental and computational investigation of the time-averaged and time-resolved pressure loading on a vaneless count-rotating turbine[R].ASME Paper 2000-GT-0445.
[2]	Haldeman C W,Dunn M G,Barter J W,et al.Experimental investigation of vane clocking in a one and 1/2 stage high pressure turbine[R].ASME Paper GT2004-53477.
[3]	Billiard N,Paniagua G,Dénos R.Effect of clocking on the heat transfer distribution of a second stator tested in a one and half stage HP turbine[R].ASME Paper GT2005-68462.
[4]	唐菲,陈党慧.1+1/2对转涡轮短周期试验台性能测试[A].中国工程热物理学会第十一届年会论文集[C].北京:热机气动热力学分卷,2005:520-526.
[5]	陈党慧,唐菲,赵晓路,等.暂冲式短周期试验台涡轮性能及不确定度分析[J].中北大学学报(自然科学版),2006,27(3):253-257.CHEN Danghui,TANG Fei,ZHAO Xiaolu,et al.Turbine performance measurement method and its uncertainty estimate on a blow-down short duration rig[J].Journal of North University of China,2006,27(3):253-257.
[6]	Povey T,Chana K S,Jones T V,et al.The effect of hot-streaks on HP vane surface and endwall heat transfer:An experimental and computational study[R].ASME Paper GT2005-69066.
[7]	Castillon L,Laroche E,Sgarzi O.Unsteady three-dimensional navier-stokes analysis of a hot streak transport through an axial high pressure turbine stage[R].ISABE 2003-1063.
[8]	Chana K S,Povey T,Terry P.The design,developmentand testing of a non-uniform inlet temperature generator for the QinetiQ transient turbine research facility[R].ASME Paper GT2003-38469.
[9]	Barringer M D,Thole K A,Polanka M D.Developing acombustor simulator for investigating high pressure turbine aerodynamics and heat transfer[R].ASME Paper GT2004-53613,2004.
[10]	Shan T,Epstein A H.Analysis of hot streak effects onturbine rotor heat load[R].ASME Paper 96-GT-118.
[11]	Weaver M M,Manwaring S R.Forcing function measurements and predictions of a transonic vaneless counter rotating turbine[R].ASME Paper 2000-GT-375.
[12]	Kielb J J,Reza S A.Experimental study of aerodynamic and structural damping in a full scale rotating turbine[R].ASME Paper 2001-GT-0262.
[13]	Kielb J J,Reza S A.Experimental and numerical study of forced response in a fullscale rotating turbine[R].ASME Paper No.2001-GT-0263.
[14]	Haldeman C W,Dunn M G,Barter J W,et al.Aerodynamic and heat-flux measurements with predictions on a modern one and 1/2 stage high pressure transonic turbine[R].ASME Paper GT2004-53478.
[15]	Smith G C,Hilditch M A.Heat transfer computations for high pressure turbine[R].ASME Paper 2001-GT-0172.
[16]	Haldeman C W,Dunn M G.Heat transfer measurements and predictions for the vane and blade of a rotating high pressure stage[R].ASME Paper GT2003-38726.
[17]	Tallman J A.CFD heat transfer predictions for a high-pressure turbine stage[R].ASME Paper GT2004-53654.
[18]	Bergholz R F,Dunn M G,Steuber G D.Rotor/stator heat transfer measurements and CFD predictions for short-duration turbine rig tests[R].ASME Paper 2000-GT-0208.
[19]	Dunn M G,Haldeman C W.Time-averaged heat flux for a recessed tip,lip,and platform of a Transonic turbine blade[R].ASME Paper 2000-GT-0197.
[20]	Chana K S,Jones T V.An investigation on turbine tip and shroud heat transfer[R].ASME Paper GT-2002-30554.
[21]	Polanka M D,Clark J P,White A L,et al.Turbine tip and shroud heat transfer and loading part B:Comparisons between prediction and measurement including insteady effects[R].ASME Paper GT-2003-38916.
[22]	Steven J,Thorpe R J,Miller.The effect of work processes on the casing heat transfer of a rotating turbine[R].ASME Paper GT2005-68437.
[23]	Didier F,Dénos R,Arts T.Unsteady rotor heat transfer in a transonic turbine stage[R].ASME Paper GT-2002-30195.
[24]	Iliopoulou V,Dénos R,Billiard N,et al.Time-averaged and time-resolved heat flux measurements on a turbine stator blade using two-layered thin-film gauges[R].ASME Paper GT2004-53437.
[25]	William A,Ainsworth R,Thorpe S.Unsteady heat transfer measurements from transonic turbine blades at engine representative conditions in a transient facility[R].ASME Paper GT2004-53835.
[26]	Keogh R C,Guenette G R,Spadaccini C M,et al.Aerodynamic performance measurements of a film-cooled turbine stage-experimental results[R].ASME Paper GT-2002-30344.
[27]	Chana K S,Hilditch M A,Anderson J.An investigation of the effects of film cooling in a high-pressure aeroengine turbine stage[R].ASME Paper GT2005-68564.
[28]	Dénos R,Arts T,Paniagua G,et al.Investigation of the unsteady rotor aerodynamics in a transonic turbine stage[R].ASME Paper 2000-GT-435.
[29]	Clark J P,Stetson G M,Magge S S,et al.The effect of airfoil scaling on the predicted unsteady loading on the blade of a 1 and 1/2 stage transonic turbine and a comparison with experimental results[R].ASME Paper 2000-GT-0446.
[30]	Valenti E,Halama J,Denos R,et al.Investigation of the 3D unsteady rotor pressure field in a HP turbine stage[R].ASME Paper GT-2002-30365.
[31]	Brian R,Green J W,Barter C,et al.Time-averaged and time-accurate aero-dynamics for the recessed tip cavity of a high-pressure turbine blade and the outer stationary shroud:domparison of computational and experimental results[R].ASME Paper GT2004-53443.
[32]	Keogh R C,Guenette G R,Sommer T P.Aerodynamic performance measurements of a fully-scaled turbine in a short duration facility[R].ASME Paper 2000-GT-486.
[33]	Atkins N R,Miller R J,Ainsworth R W.The development of aerodynamic performance measurements in a transient test facility[R].ASME Paper GT2004-53813.
[34]	Atkins N R,Ainsworth R W.The measurement of shaft power in a fully scaled transient turbine test facility[R].ASME Paper GT2005-68998.