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http://yadda.icm.edu.pl:80/baztech/element/bwmeta1.element.baztech-b9b19c4e-a016-4b8b-9659-1f94fdb38001

Czasopismo

Journal of KONES

Tytuł artykułu

Influence of selected parameters on micro gas turbine compressor design

Autorzy Czarnecki, M.  Olsen, J. 
Treść / Zawartość
Warianty tytułu
Języki publikacji EN
Abstrakty
EN The design a micro gas turbine engine is a process that requires analysis of a number of parameters. The initial stage requires consideration of more than 40 parameters [3]. The whole analysis can be made with analytical tools. However, these kinds of tools are limited to preliminary designs. After 1D-calculations and the establishment of the first CAD model, it is recommended to identify the sensitivity of the design. With a modern numerical environment such as ANSYS CFX, it is possible to predict a trend that gives the designer a 3D feedback about the initial design behaviour. For presented centrifugal compressor case, the selected parameters are vaneless diffuser space, design angle and number of stator blades. For qualitative evaluation – important results that influence design are mass flow rate, total pressure and isentropic efficiency. These results are important to turbojet engine performance and efficiency. All chosen parameters respond to given criteria. Validation and verification is still required due numerical errors that are included in CFD modelling. The advantage of 3D prediction is the possibility to eliminate gross errors before parts are sent into production.
Słowa kluczowe
EN jet engine   gas turbine   design   trend prediction   centrifugal compressor  
Wydawca Institute of Aviation
Czasopismo Journal of KONES
Rocznik 2017
Tom Vol. 24, No. 3
Strony 45--52
Opis fizyczny Bibliogr. 9 poz., rys.
Twórcy
autor Czarnecki, M.
  • Rzeszow University of Technology Department of Aircraft and Aircraft Engines Powstancow Warszawy Av. 8, 35-959 Rzeszow, Poland tel.:+48 17 8651609, fax: +48 17 8543116 , czarn@prz.edu.pl
autor Olsen, J.
  • School of Mechanical and Manufacturing Engineering The University of New South Wales Sydney, Ainsworth Building, N.S.W., 2052, Sydney, Australia tel.: +61 2 9385 5217, fax: +61 2 9663 1222 , j.olsen@unsw.edu.au
Bibliografia
[1] Avaramenko, A., Frolov, A., Hamalainen, Simulation and modelling of flow in gas compressor, Journal of Applied Mathematics, Vol. 2015.
[2] Cohen, H., Rodgers, G. F. C., Saravanamutto, H. I. H., Gas turbine theory, Longman Group limited, Essex, 1996.
[3] Czarnecki, M., Design and experimental research of microgastrubine turbojet engine,Rzeszow 2013
[4] Czarnecki, M, Micro scale gas turbine diffuser design – a practical approach, Journal of Applied Fluid Mechanics.
[5] Dixon, S. L., Hall, C. A., Fluid mechanics and thermodynamics of turbomachinery, Elsevier,Tokyo 2010.
[6] Parish, R., Wright, A., Murphy, M., Plans for the MW54 gas turbine second edition, Wren turbines LTD., August 2000.
[7] Schreckling, K., Gas Turbine Engines for Model Aircraft, Traplet Publications Limited, Worcestershire 2003
[8] Tu, J. Y., Yeoh, G. H., Liu, C., Computational Fluid Dynamics: A practical approach, Elsevier, 2012.
[9] BW, Performance turbocharger catalog 2012 Edition (BorgWarner Turbo Systems).
Uwagi
PL Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).
Kolekcja BazTech
Identyfikator YADDA bwmeta1.element.baztech-b9b19c4e-a016-4b8b-9659-1f94fdb38001
Identyfikatory
DOI 10.5604/01.3001.0010.3067