高负荷涡轮叶栅气动性能试验

杨其国; 王祥锋; 石玉文; 韩万金

高负荷涡轮叶栅气动性能试验

1.
哈尔滨电气集团公司哈尔滨汽轮机厂有限责任公司, 哈尔滨 150040
2.
哈尔滨工业大学能源科学与工程学院, 哈尔滨 150001

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- 文章访问数: 1857
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- 被引次数: 0
出版历程
- 收稿日期: 2010-12-23
- 修回日期: 2011-03-15
- 刊出日期: 2011-12-28

Experiment on aerodynamic performance of turbine static cascade with high aerodynamic loading

1.
Harbin Turbine Company Limited, Harbin Electric Corporation, Harbin 150040, China
2.
School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China

摘要

摘要: 在环形涡轮叶栅低速风洞上,对某型高负荷涡轮静叶栅进行了吹风试验.应用五孔球头测针,详细测量了在三个冲角下由栅前至栅后7个横截面内气流参数沿叶高和节距的分布.试验结果表明,沿叶高变负荷结合叶片弯曲,在满足高负荷要求的条件下能够控制边界层的集聚、转捩与分离.在主流区采用前加载叶型,保证叶片能承担高负荷.在两个端壁区采用后部加载叶型,并通过叶片正弯进一步降低气动负荷,从而减小端壁横向压力梯度,削弱端壁横向二次流.正、负冲角仅影响叶片前缘吸力面或压力面的静压分布,引起气动负荷的增加与减小.研究的高负荷涡轮叶栅具有良好的冲角适应性.
- 涡轮叶栅 /
- 高负荷 /
- 弯叶片 /
- 二次流 /
- 气动性能
Abstract: In a low-speed ring cascade wind tunnel,aerodynamic tests were fulfilled on a large enthalpy drop static cascade in the middle stage of a steam turbine.From the front to the back gate,the flow parameters in seven cross sections along the blade height and pitch at three incidences were measured in detail with the application of five-hole pin ball test.The results show that,in order to meet the requirements of high loading conditions,the combination of highly variable loading and blade bending along span-wise can control the accumulation,transition and separation of boundary layer.Fore-loaded blade profiles were applied in the main passage area to ensure that the blade could withstand high loading.After-loaded blade profile was applied to the end wall and the positive bending blade further reduced aerodynamic loading,the end wall lateral pressure gradient was cut down to weaken the end wall lateral secondary flow.Positive and negative incidences affect only the static pressure distribution at the leading edge of the suction side or pressure side,causing the increase and decrease of aerodynamic loading.The turbine cascade with high aerodynamic loading has a good adaptability of incidence.
- turbine cascade /
- high loading /
- curved blade /
- secondary flow /
- aerodynamic performance

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参考文献(17)

[1]	Pullan G,Denton J,Curtis E.Improving the performance of a turbine with low aspect ratio stators by aft-loading[R].ASME Paper GT2005-68548,2005.
[2]	Praisner T J,Allen-Bradley E,Grover E A,et al.Application of non-axisymmetric endwall contouring to conventional and high-lift turbine airfoil[R].ASME Paper GT2007-27579,2007.
[3]	Zoric T,Popovic I,Sjolander S A,et al.Comparative investigation of three highly loaded LP turbine airfoils part Ⅰ:measured profile and secondary losses at design incidence[R].ASME Paper GT2007-27537,2007.
[4]	Sonoda T,Arima T,Olhofer M,et al.A Study of advanced high loaded transonic turbine airfoils[R].ASME Paper GT2004-53773,2004.
[5]	Funazaki K,Shiba T,Tanimitsu H.Effects of blade loading distribution on aerodynamic performance of ultra-high lift LP turbine airfoils under the influences of wake passing and free-stream turbulence[R].AMSE Paper GT2010-22134,2010.
[6]	Tsujita H,Yamamoto A.Complex secondary flow and associated loss generation in ultra-highly loaded turbine cascade[R].ASME Paper GT2010-22594,2010.
[7]	Coull J D,Hodson H P.Predicting the profile loss of high-lift low pressure turbines[R].ASME Paper GT2010-22675,2010.
[8]	Howell R J,Ramesh O N,Hodson H P,et al.High lift and aft-loaded profiles for low-pressure turbines[J].Journal of Turbomachinery,2001,123(2):181-187.
[9]	Martinstetter M,Niehuis R,Franke M.Passive boundary layer control on a highly loaded low pressure turbine cascade[R].ASME Paper GT2010-22739,2010.
[10]	ZHANG Xuefeng,Vera M,Hodson H P,et al.Separation and transition control on an aft-loaded ultra-high-lift LP turbine blade at low Reynolds numbers:low-speed investigation[J].Journal of Turbomachinery,2006,128(3):517-527.
[11]	Griffin L W,Huber F W.Advancement of turbine aerodynamic design technique[R].ASME Paper 93-GT-370,1993.
[12]	Chaluvadi V S P,Kalfas A I,Hodson H P,et al.Blade row interaction in a high pressure steam turbine[R].ASME Paper 2002-GT-30574,2002.
[13]	Chaluvadi V S P,Kalfas A I,Hodson H P.Vortex transport and blade interactions in high pressure turbines[R].ASME Paper GT2003-38389,2003.
[14]	周逊.具有后部加载叶型的涡轮叶栅气动性能的试验研究[D].哈尔滨:哈尔滨工业大学,2004. ZHOU Xun.Experimental research on aerodynamic performance of turbine cascade with aft-loaded blade profile[D].Harbin:Harbin Institute of Technology,2004.(in Chinese)
[15]	熊劲松,侯安平,袁巍,等.可调叶片的发展趋势及其气动问题的探讨[J].航空动力学报,2008,23(1):112-116. XIONG Jinsong,HOU Anping,YUAN Wei,et al.Some discuss on technology trend and aerodynamics problem of adjustable blade[J].Journal of Aerospace Power,2008,23(1):112-116.(in Chinese)
[16]	Chibli H A,Abdelfattah S A,Schobeiri M T,et al.An experimental and numerical study of the effects of flow incidence angles on the performance of a stator blade cascade of a high pressure steam turbine[R].ASME Paper GT2009-59131,2009.
[17]	杨庆海.间隙、冲角及叶片弯曲对有间隙叶栅气动性能影响的试验研究[D].哈尔滨:哈尔滨工业大学,2006. YANG Qinghai.Experimental of influence of blade clearance,incidence and curving on aerodynamic performance[D].Harbin:Harbin Institute of Technology,2006.(in Chinese)