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Two-stage turbine performance improvement and noise reduction through stator-to-stator and rotor-to-rotor clocking

Wybrane pełne teksty z tego czasopisma
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Warianty tytułu
Konferencja
International Symposium SYMKOM Compressor & Turbine Flow Systems, Treory & Application Areas (15-17.09.2008; Łódź; Polska)
Języki publikacji
EN
Abstrakty
EN
In order to obtain better performances and reduction of noise emitted by modern turbomachines, the understanding of an influence of different geometry is essential. The experimental work presented in the paper is a continuation of earlier studies on effects of different geometry configurations. Till now only the stator-to-stator indexing (clocking) effect was considered. Nowadays main attention is directed to rotor-to-rotor clocking. A turbine with two identical stages was investigated. New geometry has been used. Special attention was drawn to noise emitted by the turbine due to the vane-to-vane and blade-to-blade clocking influences. It has been correlated to the overall performance (torque) of the turbine of new design and additional comparison has been done to the vane-to-vane indexing benefit. All results have been compared to the classical design positions of stators and rotors. The measurements presented in this paper have been performed at the nominal speed and at one off-design rotational speed of the machine. The rotor-to-rotor indexing turned out to be more advantageous than the stator-to-stator clocking and only a slight change in the rotor position is needed to yield higher efficiency. Similar influence has been observed for the emitted noise level. All measurements have been performed inside especially designed anechoic room.
Twórcy
  • Politechnika Lodzka Instytut Maszyn Przeplywowych
Bibliografia
  • [1] International Air Transport Association, 2004, “Environmental Review”
  • [2] Directive 2002/49/EC of the European Parliament and of the Council of 25 June 2002, “Assessment and management of environmental noise”
  • [3] Schlienger J., Kalfas A.I., Abhari R.S., 2004, „Vortex-Wake-Blade Interaction in a Shrouded Axial Turbine“, ASME GT2004-53915
  • [4] Dorney D., Sondak D., Cizmas P., 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
  • [5] Haldeman C., Krumanaker M., Dunn M., 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
  • [6] He L., Chen T., Wells R., Li Y., Ning W., 2002, “Analysis of Rotor-Rotor and Stator-Stator Interferences in Multi-Stage Turbomachines”, ASME J. of Turbomachinery, Vol. 124, pp. 564-571
  • [7] Huber F.W., Johnson P.D., Sharma O.P., Staubach J., Gaddis S., 1996, “Performance Improvement Through Indexing of Turbine Airfoils”, ASME J. of Turbomachinery, Vol. 118, pp. 630-635
  • [8] Hummel F. 2002, “Wake-Wake Interaction and Its Potential for Clocking in a Transonic HP Turbine”. J. of Turbomachinery, Vol. 124, pp. 629-635
  • [9] Jouini D., Little D., Bancalari E., Dunn M., Haldeman C., Johnson P., 2003: “Experimental Investigation of Air-foil Clocking Impacts on Aerodynamic Performance in a Two Stage Turbine Test Rig”, ASME GT2003-38872
  • [10] 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)
  • [11] Reinmoeller U., Stephan B., Schmidt S., Niehuis R., 2002, “Clocking Effects in 1.5Stage Axial Turbine”, J. of Turbomachinery, Vol.124, pp.52-60
  • [12] Koenig S., Heidecke A., Stoffel B., Fiala A., Engel K., 2004, “Clocking Effects in a 1.5-Stage Axial Turbine”, ASME GT2004-54055
  • [13] 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
  • [14] 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
  • [15] Blaszczak J.R., 2007, „Vane-To-Vane And Blade-To-Blade Indexing of a Highly-Loaded Two-Stage Turbine”, ASME GT2007-27639
  • [16] 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)
  • [17] Blaszczak, J.R., 2005, „Efficiency Improvement and Noise Reduction Through Stator-to-Stator Clocking Effect of a Two-Stage Turbine”, ASME GT2005-68833
  • [18] Blaszczak, J.R., 2006, „Noise Reduction and Efficiency Improvement through Vane Indexing of a Two-Stage Turbine”, AIAA 2006-2578
  • [19] Blaszczak, J.R., Comte-Bellot, G, Smolny, A., 2005, “New aeroacoustic facility at the Institute of Turbomachinery, Technical University of Lodz”, CMP/Turbomachinery, Vol. 128, PL, Lodz
  • [20] Krysinski J., Gallus H.E., Smolny A., Blaszczak J.R., 1995, “Axial Two-Stage Turbine Test Rig for Unsteady Flow Measurements”, CMP/Turbomachinery, Vol.108, pp.99-106
  • [21] 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, London, Vol. A, pp. 323-332
  • [22] 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
  • [23] Krysinski J., Blaszczak J.R., Smolny A., 2001, “Stator Clocking Effect on Efficiency of a Two-Stage Low-Pressure Model Turbine”. 4th EuroConf. Turbomachinery, Florence, Italy, ATI-CST090/01, pp. 1045-1051
  • [24] Krysinski J., Blaszczak J.R., Smolny A., 2003, „Two-Stage Turbine Investigations Of Unsteady Stator-Stator Interaction”, ISUAAAT’2003
  • [25] Krysinski J., Blaszczak J.R., Smolny A., 2005, „Stator Clocking Effects on 3D Flow in a Two-Stage Low-Pressure Turbine”, ASME GT2005-68811
  • [26] Smolny A., Blaszczak J.R., 1997, “Experimental Investigations of Unsteady Flow Fields In A Two-Stage Turbine”, 2nd EuroConf. on Turbomachinery, Antwerp, Belgium
  • [27] Pullan G., 2006, ”Secondary Flows and Loss Caused by Blade Row Interaction in a Turbine Stage”, J. of Turbomachinery, Vol. 128, pp. 484-491
  • [28] Pullan G., Denton J., Curtis E., 2006, ”Improving the Performance of Turbine with Low Aspect Ratio Stators by Aft-Loading”, ASME, J. of Turbomachinery, Vol. 126, pp. 492-499
  • [29] Bohn D., Ausmeier S., Ren J., 2005: “Investigation of the Optimum Clocking Position in a Two-Stage Axial Turbine”,Int. of J. Rotating Machinery, Vol.3, pp. 202-210
  • [30] Blaszczak, J.R., Kus E., 2008: „The Rotor-To-Rotor Clocking Influence On Noise Reduction Of A Two-Stage Turbine”, ISROMAC12-2008-20193
  • [31] Blaszczak, J.R., 2008: „Performance Improvement and Noise Reduction through Vane And Blade Indexing of a Two-Stage Turbine”, AIAA 2008-29
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-f027e8c9-e671-4325-8b54-71ffad7f4810
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