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Vane bowing and clocking technique influence on two-stage turbine performance

Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Konferencja
International Symposium SYMKOM Compressor & Turbine Flow Systems, Treory & Application Areas (15-17.09.2008; Łódź; Polska)
Języki publikacji
EN
Abstrakty
EN
This paper describes the experimental investigations of the clocking effects on the turbine performance characteristics. The turbine was equipped with rake temperature and pressure probes and fast response miniature pressure sensors and surface-mounted hot film sensors. To understand better an interaction mechanism and show how some flow effects can be successfully employed in estimation and correlation of stage losses, quasi-three-dimensional simulations of the airfoil clocking have been performed. Time-averaged and unsteady data including performance of particular blade/vane rows are presented and used to minimize the stage loss production due to upstream flow conditions. The results show a turbine total efficiency variation from 0.1% to 0.5%. The experiments have shown that the clocking effect seems to be mainly related to the low momentum flow region, which should be introduced into a leading edge region of the downstream vane/blade row, where the fluid momentum will be already low. Primary loss production in the blade row will be a function of the geometry and inlet time mean flow conditions and the distribution along the circumferential direction.
Twórcy
  • Institute of Turbomachinery Technical University of Lodz
autor
  • Institute of Turbomachinery Technical University of Lodz
  • Institute of Turbomachinery Technical University of Lodz
Bibliografia
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  • [2] Krysinski J., Gallus H.E., Smolny A., Blaszczak J.R., Walraevens R., 1998: “Experimental Investigation of Three Dimensional Flow In a Two-Stage Turbine”. Proc. of the VII Int. Conf. on Rotary Fluid Flow Machines, Rzeszow, Poland, pp. 215-224
  • [3] Krysinski J., Gallus H.E., Smolny A., Blaszczak J.R., 1999: “Stator Wake Clocking Effects on 3D Unsteady Flows In a Two-Stage Turbine”, 3rd EuroConf. on Turbomachinery, IMechE, C557/017/99, Vol. A, London, UK, pp. 323-332
  • [4] Krysinski J., Smolny A., Blaszczak J.R., Gallus H.E., 2000: “3D Unsteady Flow Experimental Investigations in a Two-Stage Low-Pressure Turbine”, ISUAAAT’2000, Lyon, France, pp. 515-523
  • [5] Krysinski J., Blaszczak J.R., Smolny A., 2001: “Stator Clocking Effect on Efficiency of a Two-Stage Low-Pressure Model Turbine”. 4th EuroConf. on Turbomachinery, ATI-CST090/01, pp. 1045-1051, Florence, Italy
  • [6] Krysinski J., Blaszczak J.R., Smolny A., 2003: “Experimental and Numerical Investigation of the 3D Steady and Unsteady Flow Through Turbine Stages”, Polish State Committee for Scientific Research, Final Report of the Project # 1672/T10/2000/19 (in Polish).
  • [7] Krysinski J., Blaszczak J.R., Smolny A., 2005: „Stator Clocking Effects on 3D Flow in a Two-Stage Low-Pressure Turbine”, ASME GT2005-68811
  • [8] Eulitz F., 2000: “Modelling and Simulation of Transition Phenomena in Unsteady Turbomachinery Flow”, ISUAAAT 2000, Lyon, France
  • [9] Howell, R.J., Ramesh, O.N., Hodson, H.P., Harvey, N.W., Schulte, V., 2001: “High Lift and Aft-Loaded Profiles for Low-Pressure Turbines”, ASME J. of Turbomachinery, Vol. 123, pp. 181-188
  • [10] Reynolds, W. C., Alonso J.J., Fatica M., 2003: “Aircraft Gas Turbine Engine Simulations”, AIAA2003-3698
  • [11] Dossena V., D’Ippolito G., Pesatori E., 2004: “Stagger Angle and Pitch-Cord Ratio Effects on Secondary Flows Downstream of a Turbine Cascade at Several Off-Design Conditions”, ASME GT2004-54083
  • [12] Benner M., Sjolander S., Moustapha S., 2004: „Measurements of Secondary Flows of a turbine Cascade at Off-Design Incidence“, ASME GT2004-53786
  • [13] Arnone A., Bonaiuti D., Focacci A., Pacciani R., Del Greco A. S., Spano E., 2004: “Parametric Optimization of a High-Lift Turbine Vane“, GT2004-54308
  • [14] Stieger R.D., Hodson H.P., 2003: „The Transition Mechanism of Highly-Loaded LP Turbine Blades“, ASME GT2003-38304
  • [15] Schobeiri M., Ozturk B., 2004: “Experimental Study of the Effect of Periodic Unsteady Wake Flow on Boundary Layer Development, Separation, and Re-Attachment Along the Surface of a Low Pressure Turbine Blade”, ASME GT2004-53929
  • [16] Schlienger J., Kalfas A.I., Abhari R.S., 2004: „Vortex-Wake-Blade Interaction in a Shrouded Axial Turbine“, ASME GT2004-53915
  • [17] Dorney D.J., Sondak D.L., Cizmas P.G.A., Saren V.E., Savin N.M., 1999: “Full-Annulus Simulations of Airfoil Clocking in a 1-1/2 Stage Axial Compressor”. ASME 99-GT-023
  • [18] Haldeman C.W., Krumanaker M.L., Dunn M.G., 2003: “Influence of Clocking and Vane/Blading Spacing on the Unsteady Surface Pressure Loading for a Modern Stage and One-Half Transonic Turbine”, ASME GT2003-38724
  • [19] He L., Chen T., Wells R.G., Li Y.S., Ning W., 2002: “Analysis of Rotor-Rotor and Stator-Stator Interferences in Multi-Stage Turbomachines”, ASME J. of Turbomachinery, Vol. 124, pp. 564-571
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  • [21] Hummel F. 2002: “Wake-Wake Interaction and Its Potential for Clocking in a Transonic HP Turbine”. ASME J. of Turbomachinery, Vol. 124, pp. 69-635
  • [22] Jouini D.B.M., Little D., Bancalari E., Dunn M., Haldeman C., Johnson P.D., 2003: “Experimental Investigation of Airfoil Clocking Impacts on Aerodynamic Performance in a Two Stage Turbine Test Rig”, ASME GT2003-38872
  • [23] Saren V.E., Savin N.M., 2000: “Hydrodynamic Interaction of a Stator-Rotor-Stator System of an Axial Turbomachine”, Fluid Mechanics 3/2000, Russian Academy of Sciences, Moscow, pp. 145-158 (in Russian)
  • [24] Reinmoeller U., Stephan B., Schmidt S., Niehuis R., 2002: “Clocking Effects in a 1.5 Stage Axial Turbine – Steady and Unsteady Experimental Investigations Supported by Numerical Simulations”, ASME, J. of Turbomachinery, Vol. 124, pp. 52-60
  • [25] Koenig S., Heidecke A., Stoffel B., Fiala A., Engel K., 2004: “Clocking Effects in a 1.5-Stage Axial Turbine - Boundary Layer Behaviour at Midspan”, ASME GT2004-54055
  • [26] Gadea J., Denos R., Paniagua G., Billiard N., Sieverding C.H., 2004: “Effect of Clocking on the Second Stator Pressure Field of a One and a Half Stage Transonic Turbine”, ASME GT2004-53463
  • [27] Haldeman C.W., Dunn M.G., Barter J.W., Green B.R., Bergholz R.F., 2004: “Experimental Investigation of a Vane Clocking in a One and ½ Stage HP Turbine”, ASME GT2004-53477
  • [28] Smolny A., Blaszczak J.R., 1997: “Experimental Investigations of Unsteady Flow Fields in a Two-Stage Turbine”, 2nd EuroConf. on Turbomachinery, Antwerp, Belgium
  • [29] Blaszczak J.R., 2005: „Experimental Investigations of a Turbine Stage Load on Boundary Layers and Noise Generation”, Polish State Committee for Scientific Research, Scientific Project # 4T10B04323 (in Polish)
  • [30] Blaszczak J.R., 2005: „Efficiency Improvement and Noise Reduction Through Stator-Stator Clocking Effect of a Two-Stage Turbine”, ASME GT2005-68833
  • [31] Blaszczak J.R., 2006: “Noise Reduction and Efficiency Improvement through Vane Indexing of a Two-Stage Turbine”, AIAA-2006-2578
  • [32] Pullan G., 2006: ”Secondary Flows and Loss Caused by Blade Row Interaction in a Turbine Stage”, J. of Turbomachinery, Vol. 128, pp. 484-491
  • [33] Bohn D., Ausmeier S., Ren J., 2005: “Investigation of the Optimum Clocking Position in a Two-Stage Axial Turbine”, Int. J. of Rotating Machinery, Vol. 3, pp. 202-210
  • [34] Denton J.D., 1993: “Loss Mechanisms in Turbomachines”, ASME J. of Turbomachinery, Vol. 115, pp. 621-656
  • [35] Harrison S., 1990: “Secondary Loss Generation in a Linear Cascade of High-Turning Turbine Blades”, J. of Turbomachinery, Vol. 112, pp. 618-624
  • [36] Pullan G., Denton J., Curtis E., 2006: ”Improving the Performance of Turbine with Low Aspect Ratio Stators by Aft-Loading”, ASME J. Turbomachinery Vol. 126, pp. 492-4
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-8a936dc3-400e-4f87-9787-d92c493d96d4
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