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Flow noise correlation with efficiency and vibration level - two-stage turbine case

Identyfikatory
Warianty tytułu
PL
Badanie korelacji hałasu, przepływu, sprawności oraz poziomu drgań dla przypadku dwustopniowej turbiny
Języki publikacji
EN
Abstrakty
EN
The objective of the presented test program was to investigate flow effects influence on the performance, noise and vibration levels of a two-stage low-pressure turbine. Measurement results for different circumferential positions of the turbine vanes are described to determine how noise and vibration could be affected by airfoil indexing and flow condition changes. Two cases are presented: for nominal rotational speed of the machine and for off-design turbine conditions (highly-loaded turbine case). Results showed some possibilities of a future turbomachinery performance and reliability improvement. In addition, another way to reduce noise emitted by a turbomachine and to lower vibration level is demonstrated. The investigations have been carried out at the Institute of Turbomachinery (Instytut Maszyn Przepływowych, IMP), Technical University of Lodz, Poland.
Rocznik
Strony
8--15
Opis fizyczny
bibliogr. 16 poz.
Twórcy
  • Politechnika Łódzka, Instytut Maszyn Przepływowych, 1-10, ul. Wólczańska 219/223, 93-005 Łódź
Bibliografia
  • [I] HUMMEL F. 2002, Wake-Wake Interaction and Its Potential for Clocking in a Transonic HP Turbine. ASME J. of Turbomachinery, Vol. 124, pp. 629-635.
  • [2] REINMOELLER U., STEPHAN B., SCHMIDT S., NIEHUIS R., 2002, Clocking Effects in a 1.5 Stage Axial Turbine, ASME, J. Turbomachinery, Vol. 124.
  • [3] KOENIG S., HEIDECKE A., STOFFEL B., FIALA A., ENGEL K., 2004, Clocking Effects in a 1.5 Stage Turbine, ASME GT2004-54055.
  • [4] HALDEMAN C.W., KRUMANAKER M.L., DUNN M.G., 2003, Influence of Clocking and Vane/Blade Spacing on the Unsteady Surface Pressure Loading for a Modern Stage and One-Half Transonic Turbine, ASME 2003-38724.
  • [5] 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 „Stage High Pressure Turbine, ASME GT2004-53477.
  • [6] JOUINI D., LITTLE D., BANCALARI E., DUNN M., HALDEMAN C, JOHNSON P., 2003: Experimental Investigation of Airfoil Clocking Impacts on Aerodynamic Performance in a Two Stage Turbine Test Rig, ASME GT2003-38872.
  • [7] KRYSINSKI J.E., GALLUS H.E., SMOLNY A., BLASZCZAK J.R., 1995, Axial Two-Stage Turbine Test Rig for Unsteady Flow Measurements, SYMKOM'95, CMP-Turbomachinery, Vol. 108, TU Lodz.
  • [8] SMOLNY A., BLASZCZAK J.R., 1997, Experimental Investigations of Unsteady Flow Fields in a Two-Stage Turbine, 2nd European Conference on Turbomachinery, Antwerp, Belgium.
  • [9] 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, pp.323-332, London.
  • [10] KRYSINSKI J., BLASZCZAK J.R., SMOLNY A., 2001, Stator Clocking Effect on Efficiency of a Two-Stage LP Turbine. 4th EuroConf. on Turbomachinery, ATI-CST090/01, pp. 1045-1051, Florence, Italy.
  • [11] KRYSINSKI J., SMOLNY A., BLASZCZAK J., GALLUS H.E., 2000, 3D Unsteady Flow Experimental Investigations in a Two-Stage LP Turbine, ISUAAAT'2000, Lyon, France, pp. 515-523.
  • [12] KRYSINSKI J.E., BLASZCZAK J.R., SMOLNY A., 2005, Stator Clocking Effects on 3D Flow in a Two-Stage LP Turbine, ASME GT2005-68811.
  • [13] BLASZCZAK J., 2005, Experimental Investigations of a Turbine Stage Load on Boundary Layers and Noise Generation, Polish State Committee for Scientific Research, Scientific Project #4T10B04323.
  • [14] BLASZCZAK J.R., 2005, Efficiency Improvement and Noise Reduction through Stator-Stator Clocking Effect of a Two-Stage Turbine, ASME GT2005-68833.
  • [15] 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, pp.79-86.
  • [16] BLASZCZAK J.R., 2006, Noise Reduction and Efficiency Improvement through Vane Indexing of a Two-Stage Turbine, AIAA 2006-2578.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPW8-0002-0061
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