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The assessment of the calculation method for determining characteristics of one straight fin labyrinth sea

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The method for the selection of a calculation scheme for the evaluation of the flow behaviour of labyrinth seal with one straight fin, against smooth wall, was presented. Experimental results were obtained from measurement data carried out on the in house, vacuum test section. The advantage of the test rig is a circular shape of the labyrinth specimen, providing similar shape to configuration operated in practise. In computational fluid dynamics study different types of mesh resolution were tested, with variable volume discretization in the area of a labyrinth fin tip. Moreover, a wide range of turbulence models basing on k-ε and k-ω, exploiting the (Reynolds Average Navier Stokes) scheme, for the flow pattern evaluation, were examined. All obtained results were compared with literature data, covering research conducted on similar configurations. The presented study shows challenges as well as the possibilities of calculation simplification and compares results obtained by means of simulations and experiment. The proposed method is characterised by excellent agreement of computational results with experiment data.
Rocznik
Tom
Strony
89--107
Opis fizyczny
Bibliogr. 15 poz., rys., tab.
Twórcy
  • Silesian University of Technology, Institute of Power Engineering and Turbomachinery, Konarskiego 20, 44-100 Gliwice, Poland
autor
  • Silesian University of Technology, Institute of Power Engineering and Turbomachinery, Konarskiego 20, 44-100 Gliwice, Poland
autor
  • Silesian University of Technology, Institute of Power Engineering and Turbomachinery, Konarskiego 20, 44-100 Gliwice, Poland
autor
  • Silesian University of Technology, Institute of Power Engineering and Turbomachinery, Konarskiego 20, 44-100 Gliwice, Poland
Bibliografia
  • [1] Steinetz B.M., Hendricks R.C., Munson J.: Advanced seal technology role in meeting next generation turbine engine goals. AC/322(AVT)TP/9RTO, Paper RTO–MP–8, 1999.
  • [2] Hendricks R.C., Steinz B.M., Braun M.J.: Turbomachine sealing and secondary flows. Part 1 – Review of sealing performance, customer, engine designer, and research issues.’ NASA/TM—2004-211991/PART1, 2004.
  • [3] R. Paolio, Moore S., Cloud D., Glahn J.A.: Impact of rotational speed on the discharge characteristic of stepped labyrinth seals. Conf.: ASMETurbo Expo2007, DOI:10.1115/GT200728248, 2007.
  • [4] Denecke J., Dullenkopf K., Wittig S., Bauer H.: Experimental investigation of the total temperature increase and swirl development in rotating labyrinth seals. In: Proc. ASME Turbo Expo 2005 Power for Land, Sea and Air, GT2005-68677, 2005.
  • [5] Massini D., Facchini B., Micio M., Bianchini C., Ceccherini A., Innocenti L.: Analysis of flat plate honeycomb seals aerodynamic losses: effects of clearance. In: 68th Conf. Italian Thermal Machines Engineering Association, ATI2013, Energy Procedia 45(2014), 502–511.
  • [6] Doerr L.: Modellmessungen und Berechnungen zum Durchflussverhalten von Durchblicklabyrinthen unter Berĺucksichtigung der ĺUbertragbarkeit. PhD thesis, Institut für Thermische Stromungsmaschinen, Universitat Karlsruhe (TH), 1985.
  • [7] Braun E., Dullenkopf K., Bauer H.J.: Optimization of labyrinth seal performance combining experimental, numerical and data mining methods. ASME Paper GT2012-68077, 2012.
  • [8] Bochon K.: Numerical investigation of fluid flow and heat transfer phenomena in selected parts of the gas turbine stage. PhD thesis, Gliwice, 2012.
  • [9] Ansys CFX - Use guide tutorial 9..
  • [10] Dong-Chun C., Rhode D.: Development of a two-dimensional computational fluid dynamics approach for computing three-dimensional honeycomb labyrinth leakage. Trans. ASME, 126(2004), 794–802.
  • [11] Alizadeh M., Nikkhahi B., Farahani A.S., Fathi A.: Numerical study on the effect of geometrical parameters on the labyrinth-honeycomb seal performance. ASME Paper GT201425147, 2014.
  • [12] Snow E.W.: Diskussionsbeitrag. Proc. Inst. Mech. Engrs. 166(1952).
  • [13] Stocker H.L.: Determining and Improving Labyrinth Seal Performance in Current and Advanced High Performance Gas Turbines. AGARDCP-273, 1978.
  • [14] Zimmermann H., Wolff K.H.: Air System Correlations Part 1: Labyrinth Seals. Trans. ASME 1998.
  • [15] Ansys CFX 16.2 User Guide.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a01d9c58-8d9f-41f9-ad64-75cb88dab4ea
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