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Modernization of a high pressure synthesis gas turbocompressor

Treść / Zawartość
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper describes several modernization aspects of a three-staged synthesis gas radial turbo compressor. The principal aim was to adapt the machine to new working conditions, resulting from the current state-of-art production technology. The required discharge pressure was changed from 21.1 MPa to 14 MPa. The paper covers the discussion on the scope of modernization, its variants and the final variant choice. It provides review of the thermodynamic calculation methodology, dedicated test stand results and also some of the on-site acceptance tests. The revamped compressor is in continuous service since October 2015.
Słowa kluczowe
Rocznik
Tom
Strony
121--130
Opis fizyczny
Bibliogr. 18 poz., rys.
Twórcy
  • Lodz University of Technology, Institute of Turbomachinery, 219/223 Wólczańska, 93-005 Łódź, Poland
autor
  • NEO-TEC Sp. z o.o., Kobiałka 11a, 09-411 Płock, Poland
autor
  • NEO-TEC Sp. z o.o., Kobiałka 11a, 09-411 Płock, Poland
autor
  • Lodz University of Technology, Institute of Turbomachinery, 219/223 Wólczańska, 93-005 Łódź, Poland
Bibliografia
  • [1] Benvenuti E.: Research on centrifugal compressor stages with low flow coefficients. Quaderni Pignone 15(1972), 11–19.
  • [2] Biba Y.I., Nye D.A., Zheji L.L.U.: Performance evaluation and fluid flow analysis in low flow stages of industrial centrifugal compressor. Int. J. Rotat. Mach. 8(2002), 5, 309–317.
  • [3] O’Connor J.: Uprating feasibility studies for turbocompressors in refinery and chemical processes-improving existing equipment. Sulzer Techn. Rev. 3(2007), 10–13.
  • [4] Jansen W.: Rotating stall in a radial vaneless diffuser. J. Basic Eng. 86(1964), 4, 750–758.
  • [5] Kabałyk K., Kryłłowicz W.: Numerical modeling on the performance of a centrifugal compressor impeller with low inlet flow coefficient Transactions IFFM, 131(2016), 41–53.
  • [6] Kozanecki Z.: Rotating Systems of the Low and Medium Power Turbomachinery. ITE Publ. House, Łódź-Radom 2008 (in Polish).
  • [7] Kozanecki Z., Kryłłowicz W.: Analysis of technical modernization possibilities of the synthesis gases compressor C1501–C1502 in Anwil SA Ammonia Plant, part I, part II. Opinion on the viability of already operating machine in conditions of cooperation with the new converter D 160, Łódź 2012 (in Polish).
  • [8] Kozanecki Z., Kryłłowicz W., Świder P., Kozanecki Z. jr: Complex modernization of large size industrial process compressors-technical aspects and examples. [In :] Proc. VETOMAC VIII Int. Conf. on Vibration Engineering and Technology of Machinery, R. Rzadkowski (Ed.), Wydawnictwo IMP PAN, Gdańsk 2012, 155–166.
  • [9] Kryłłowicz W., Kozanecki Z.: Complex modernization of the ammonia compressor. ZN PŁ, CMP, 133, Łódź 2008, 165–174.
  • [10] Kryłłowicz W., Kozanecki Z., Świder P.: Modernization of a nitrous gas turbine – driven turbocomressor. Mechanics and Mechanical Eng. 15(2011), 3, 273–288.
  • [11] Kryłłowicz W.: Theory and practice of modernization of the radial compressor. Monografie Politechniki Łódzkiej, Łódź 2013 (in Polish).
  • [12] Lindner P.: Aerodynamic tests on centrifugal process compressors – influence of diffusor diameter ratio, axial stage pitch and impeller cutback. ASME J. Eng. Power-T ASME 105(1983), 4, 910–919.
  • [13] Luedtke K.H.: Process Centrifugal Compressors. Basics Function, Operation, Design, Application. Springer, Berlin Heidelberg 2004.
  • [14] Muenger F., Naef C.: Neues Innenleben fuer bestehende Verdichter, Sulzer Techn. Rev. 1(2000), 28-31.
  • [15] Paroubek J., Cyrus V., Kynel J.: Experimental investigation and performance analysis of six low coefficient centrifugal compressor stages. J. Turbomach 117(1995), 4, 585–592.
  • [16] Świder P., Kozanecki Z., Graczykowski M., Kryłłowicz W.: Technical aspects of a large size industrial process turbocompressor revamp. Open Eng. 5(2015), 1, 438–446.
  • [17] Yongsheng Wang, Feng Lin, Chaogun Nie: Design and performance evaluation of a very low flow coefficient centrifugal compressor. Int. J. Rotat. Mach. 2013(2013), ID 293486.
  • [18] Ansys website (2015), www.ansys.com , (accessed on 15 March, 2015).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-4b409e4b-7c34-4f1e-89df-b546138b1674
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