Zusammenfassung
Die instationäre und dreidimensionale Strömung durch die Verdichterbeschaufelung ist bei der Auslegung der Kanalgeometrie zu berücksichtigen. Die Auslegung der Beschaufelung mit großem Streckungsverhältnis legt zwar die Trennung in die Beschreibung der Kanalströmung als Kaskade und als Meridianströmung nahe, wie von Wu [1] eingeführt wurde. Mit geringeren Streckungsverhältnissen ist die dreidimensionale Wechselwirkung bei dieser getrennten Behandlung jedoch immer schlechter beschreibbar. Bei hohen Belastungen der Profile können die Eckenwirbel aufgrund des umfangsmäßigen Druckgradienten zwei Drittel der Kanalhöhe umfassen, so dass die Blockage und die Verluste stark ansteigen.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Literatur
Wu C-H (1952) A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial-, radial-, and mixed-flow types, NACA TN 2604
Hoeger M, Sievers N, Lawerenz M (2001) On the performance of compressor blades with contoured endwalls. In: Proceedings of 4th european conference on turbomachinery: fluid dynamics and thermodynamics, Florence, Italy, S 711–722.
Chen PP, Qiao WY, Hashimu SFA, Shi PJ, Zhao L (2011) Passive control of hub-corner separation/stall using axisymmetric-Hub contouring. Proc Inst Mech Eng G J Aerosp Eng 226(10):1214–1224
Reising S, Schiffer HP (2009) Non-axisymmetric end wall profiling in transonic compressors. part 1: improving the static pressure recovery at off-design conditions by sequential hub and shroud end wall profiling. In: Proceedings of ASME Turbo Expo 2006: power for land, sea, and air, Bd 6: turbomachinery, parts A and B, paper GT2009-59133, Barcelona, Spain, 8–11 May
Li X, Chu W, Wu Y (2014) Numerical investigation of inlet boundary layer skew in axial-flow compressor cascade and the corresponding non-axisymmetric end wall profiling. Proc Inst Mech Eng A J Power Energy 228(6):638–656
Zhang Y, Li J, Ji L (2017) Numerical research on effects of shroud concentration on tip leakage flow and overall performance of axial compressors. In: Proceedings of ASME Turbo Expo 2017: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2017-63468, Charlotte, USA, 26–30 June
Harvey NW (2008) Some effects of non-axisymmetric endwall profiling on axial flow compressor aerodynamics, part I: linear cascade investigation. In: Proceedings of ASME Turbo Expo 2008: power for land, sea, and air, Bd 6: turbomachinery, parts A, B, and C, paper GT2008-50990, Berlin, Germany, 9–13 June
Harvey NW, Offord TP (2008) Some effects of non-axisymmetric endwall profiling on axial flow compressor aerodynamics, part II: multi-stage HPC CFD-study. In: Proceedings of ASME Turbo Expo 2008: power for land, sea, and air, Bd 6: turbomachinery, parts A, B, and C, Paper GT2008-50991, Berlin, Germany, 9–13 June
Reising, S (2011) Steady and unsteady performance of a transonic compressor stage with non-axisymmetric end walls. PhD thesis, TU Darmstadt
Nerger D, Saathoff H, Radespiel R, Gümmer V, Clement C (2012) Experimental investigation of endwall and suction side blowing in a highly loaded compressor stator cascade. ASME J Turbomach 134(2):021010
Hecklau M, Gmelin C, Nitsche W, Thiele F, Huppertz A, Swoboda M (2011) Experimental and numerical results of active flow control on a highly loaded stator cascade. Proc Inst Mech Eng A J Power Energy 225(7):907–918
Gill A, von Backström TW, Harms TM (2014) Flow fields in an axial flow compressor during four-quadrant operation. ASME J Turbomach 136(6):061007
Dorfner C, Nicke E, Voss C (2007) Axis-asymetric profiled endwall design using multiobjective optimization linked with 3D RANS-flow-simulations. In: Proceedings of ASME Turbo Expo 2007: power for land, sea, and air, Bd 6: Turbo Expo 2007, parts A and B, paper GT2007-27268, Montreal, Canada, 14–17 May 2007
Hoynacki A (1999a) Einfluss von instationärer Strömung und Turbulenz auf die Grenzschicht und auf die Druckverteilungen von Beschaufelungen moderner mehrstufiger Verdichter. Abschlussbericht Vorhaben Nr. 601, Forschungsvereinigung Verbrennungskraftmaschinen e. V.
Hoynacki A (1999b) Experimentelle Untersuchung instationärer Strömungsvorgänge in einem dreistufigen Axialverdichter mit CDA-Beschaufelung. Dissertation, Institut für Strahlantriebe und Turbomaschinen, RWTH Aachen
Bohne A (2001) Mehrstufiger Axialverdichter mit CDA-Beschaufelung. Abschlussbericht Vorhaben Nr. 694, Forschungsvereinigung Verbrennungskraftmaschinen e. V.
Heinichen F, Gümmer V, Plas A, Schiffer HP (2011) Numerical investigation of the influence of non-axisymmetric hub contouring on the performance of a shrouded axial compressor stator. CEAS Aeronaut J 2(1):89–98
Harvey NW (2008) Some effects of non-axisymmetric end wall profiling on axial flow compressor aerodynamics. Part I: linear cascade investigation. In: Proceedings of ASME Turbo Expo 2008: power for land, sea, and air, Bd 6: turbomachinery, parts A, B, and C, paper GT2008-50990, Berlin, Germany, 9–13 June
Hergt A, Meyer R, Liesner K, Nicke E (2011) A new approach for compressor endwall contouring. In: Proceedings of ASME 2011 Turbo Expo: turbine technical conference and exposition, Bd 7: turbomachinery, parts A, B, and C, paper GT2011-45858, Vancouver, British Columbia, Canada, 6–10 June
Dorfner C, Hergt A, Nicke E, Moenig R (2010) Advanced non-axisymmetric endwall contouring for axial compressors by generating an aerodynamic separator – part I: principal cascade design and compressor application. ASME J Turbomach 122(2):021026
Reutter O, Hervé S, Nicke E (2009) Automated optimization of the non-axisymmetric hub endwall of the rotor of an axial compressor. In: Proceeding of the 10th European conference on turbomachinery, Lappeenranta, Finland, S 1–11
Yi W, Li J, Yu J, Ji L (2016) Investigation on the effect of streamwise grooves on controlling corner flow separation. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-58141, Seoul, South Korea, 13–17 June
Lei V-M, Spakovszky ZS, Greitzer EM (2008) A criterion for axial compressor hub-corner stall. ASME J Turbomach 130(3):031006
Obaida HMB, Kawase M, Rona A, Gostelow JP (2016) Some perspectives on the treatment of three-dimensional flows on axial compressor blading. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-57617, Seoul, South Korea, 13–17 June
Goinis G, Nicke E (2016) Optimizing surge margin and efficiency of a transonic compressor. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-7896, Seoul, South Korea, 13–17 June
Greitzer EM, Nikkanen JP, Haddad DE, Mazzawy RS, Joslyn HD (1979) A fundamental criterion for the application of rotor casing treatment. ASME J Fluids Eng 101:237–243
Wilke I, Kau H-P (2004a) A numerical investigation of the flow mechanisms in a HPC front stage with axial slots. ASME J Turbomach 126:339
Wilke I, Kau H-P (2004b) Stall margin enhancing flow mechanisms in a transonic compressor stage with axial slots. In: Proceedings of the 10th of ISROMAC 2004, paper ISROMAC10-2004-006, Honolulu, Hawaii, 7–11 March
Wilke I, Kau H-P (2001) Wechselwirkung zwischen Rotorströmung und Casing Treatment. DGLR Jahrestagung, DGLR-JT2001-084
Wilke I, Kau H-P (2002) A numerical investigation of the influence of casing treatments on the tip leakage flow in a HPC front stage. In: Proceedings of ASME Turbo Expo 2002: power for land, sea, and air, Bd 5: Turbo Expo 2002, parts A and B, paper GT2002-30642, Amsterdam, The Netherlands, 3–6 June
Wilke I, Kau H-P (2003) A numerical investigation of the flow mechanisms in a HPC front stage with axial slots. In: Proceedings of ASME Turbo Expo 2003, collocated with the 2003 international joint power generation conference, Bd 6: Turbo Expo 2003, parts A and B, paper GT2003-38481, Atlanta, Georgia, USA, 16–19 June
Hofmann W, Ballmann J (2002) Tip clearance vortex development and shock-vortex-interaction in a transonic axial compressor rotor. In: Proceedings of 40th AIAA aerospace sciences meeting & exhibit, paper AIAA 2002-0083, Reno, NV, USA, 14–17 January
Hofmann W, Ballmann J (2003) Some aspects of tip vortex behavior in a transonic turbo compressor. Conference Paper ISABE-2003-1223
Schlechtriem S, Lötzerich M (1997) Breakdown of tip leakage vortices in compressors at flow conditions close to stall. In: Proceedings of ASME 1997 international gas turbine and aeroengine congress and exhibition, Bd 1: aircraft engine; marine; turbomachinery; microturbines and small turbomachinery, paper 97-GT-041, Orlando, Florida, USA, 2–5 June
Furukawa M, Inoue M, Saiki K, Yamada K (1998) The role of tip leakage vortex breakdown in compressor aerodynamics. In: Proceedings of ASME 1998 international gas turbine and aeroengine congress and exhibition, Bd 1: turbomachinery, paper 98-GT-239, Stockholm, Sweden, 2–5 June
Hoeger M, Fritsch G, Bauer D (1998) Numerical simulation of the shock tip leakage vortex interaction in a HPD-front stage. In: Proceedings of ASME 1998 international gas turbine and aeroengine congress and exhibition, Bd 1: turbomachinery, paper 98-GT-261, Stockholm, Sweden, 2–5 June
Takata H, Tsukuda Y (1977) Stall margin improvement by casing treatment – its mechanism and effectiveness. ASME J Eng Power 99(1):121–133
Shabir A, Adamczyk IJ (2004) Flow mechanism for stall margin improvement due to circumferential casing grooves on axial compressors. In: Proceedings of ASME Turbo Expo 2004: power for land, sea, and air, Bd 5: turbo Expo 2004, parts A and B, paper GT2004-53903, Vienna, Austria, 14–17 June
Zhu J, Wu Y, Chu W (2005) Axial location of casing treatment in multistage axial flow compressor. In: Proceedings of ASME Turbo Expo 2005: power for land, sea, and air, Bd 6: turbo Expo 2005, parts A and B, paper GT2005-69105, Reno, Nevada, USA, 6–9 June
Choi K-J, Kim J-H, Kim K-Y (2010) Design optimization of circumferential casing grooves for a transonic axial compressor to enhance stall margin. In: Proceedings of ASME Turbo Expo 2010: power for land, sea, and air, Bd 7: turbomachinery, parts A, B, and C, paper GT2010-22396, Glasgow, UK, 14–18 June, S 1–9
Carnie G, Wang Y, Qin N, Shahpar S (2011) Design optimisation of casing grooves using the zipper layer meshing method. In: Proceedings of ASME 2011 Turbo Expo: turbine technical conference and exposition, Bd 7: turbomachinery, parts A, B, and C, paper GT2011-45483, Vancouver, British Columbia, Canada, 6–10 June
Houghton T, Day IJ (2011) Enhancing the stability of subsonic compressors using casing grooves. ASME J Turbomach 133(2):021007
Houghton T, Day IJ (2012) Stability enhancement by casing grooves: the importance of stall inception mechanism and solidilty. ASME J Turbomach 134(2):021003
Zhang HG, Tan F, Wu YH, Chu WL, Wang W (2016) Experimental and numerical investigation of effect of center offset degree on compressor stability with circumferential grooved casing treatment. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-56757, Seoul, South Korea, 13–17 June
Rabe DC, Hah C (2002) Application of casing circumferential grooves for improved stall margin in a transonic axial compressor. In: Proceedings of ASME Turbo Expo 2002: power for land, sea, and air, Bd 5: Turbo Expo 2002, parts A and B, paper GT2002-30641, Amsterdam, The Netherlands, 3–6 June, S 1141–1153
Perrot V, Touyeras A, Lucien G (2007) Detailed CFD analysis of a grooved casing treatment on an axial subsonic compressor. In: Proceedings of the 7th European conference on turbomachinery, S 305–316
Müller MW, Schiffer H-P, Hah C (2007) Effect of circumferential grooves on the aerodynamic performance of an axial single-stage transonic compressor. In: Proceedings of ASME Turbo Expo 2007: power for land, sea, and air, Bd 6: Turbo Expo 2007, parts A and B, paper GT2007-27365, Montreal, Canada, 14–17 May
Müller MW, Biela C, Schiffer H-P (2008) Interaction of rotor and casing treatment flow in an axial single-stage transonic compressor with circumferential groove. In: Proceedings of ASME Turbo Expo 2008: power for land, sea, and air, Bd 6: turbomachinery, parts A, B, and C, paper GT2008-50135, Berlin, Germany, 9–13 June
Wu Y, Chu W, Zhang H, Li Q (2010) Parametric investigation of circumferential grooves on compressor rotor performance. ASME J Fluids Eng 132(12):121103
Johann E, Nipkau J, Muck B (2008) Experimental and numerical flutter investigation of the 1st stage rotor in 4-stage high speed compressor. In: Proceedings of ASME Turbo Expo 2008: power for land, sea, and air, Bd 5: structures and dynamics, parts A and B, paper GT2008-50698, Berlin, Germany, 9–13 June
Souleimani Y, Vo HD, Yu H (2018) Performance desensitization for a high-speed axial compressor. In: Proceedings of ASME Turbo Expo 2018: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2018-77203, Oslo, Norway, 11–15 June
Rolfes M, Lange M, Vogeler K, Mailach R (2017) Experimental and numerical investigation of a circumferential groove casing treatment in a low speed axial research compressor at different tip clearances. In: Proceedings of ASME Turbo Expo 2017: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2017-63051, Charlotte, USA, 26–30 June
Guinet C, Streit JA, Gümmer V, Kau H-P (2014) Tip gap variation on a transonic rotor in the presence of tip blowing. In: Proceedings ASME Turbo Expo 2014: turbine technical conference and exposition, Bd 2A: turbomachinery, paper GT2014-25042, Düsseldorf, Germany, 16–20 June
Azmian AR, Elder R, Mcenzie AB (1990) Application of recess vaned casing treatment to axial flow fans. ASME J Turbomach 112(1):145–150
Smith GDJ, Cumpsty NA (1984) Flow phenomena in compressor casing treatment. ASME J Eng Gas Turbines Power 106(3):532–541
Wilke I, Kau H-P (2005) Numerically aided design of a high-efficient casing treatment for a transonic compressor. In: Proceedings of ASME Turbo Expo 2005: power for land, sea, and air, Bd 6: Turbo Expo 2005, parts A and B, paper GT2005-68993, Reno, Nevada, USA, 6–9 June
Ma N, Nan X, Lin F (2016) Numerical study on effects of axial-slot casing treatment on peak efficiency of axial compressors. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-56554, Seoul, South Korea, 13–17 June
Denton JD (1993) The 1993 IGTI scholar lecture: loss mechanisms in turbomachines. ASME J Turbomach 115(4):621–656
Lu X, Chu W, Zhu J, Wu Y (2006a) Mechanism of the interaction between casing treatment and tip leakage flow in a subsonic axial compressor. In: Proceedings of ASME Turbo Expo 2006: power for land, sea, and air, Bd 6: turbomachinery, parts A and B, paper GT2006-90077, Barcelona, Spain, 8–11 May
Müller MW, Schiffer H-P, Voges M, Hah C (2011) Investigation of passage flow features in a transonic compressor rotor. In: Proceedings of ASME 2011 Turbo Expo: turbine technical conference and exposition, Bd 7: turbomachinery, parts A, B, and C, paper GT2011-45364, Vancouver, British Columbia, Canada, 6–10 June, S 65–75
Lu X, Chu W, Zhu J, Wu Y (2006) Experimental und numerical investigation of a subsonic compressor with bend skewed slot casing Treatment. In: Proceedings of ASME Turbo Expo 2006: power for land, sea, and air, Bd 6: turbomachinery, parts A and B, paper GT2006-90026, Barcelona, Spain, 8–11 May
Emmerich R, Hönen H, Niehuis R (2007a) Time resolved investigations of an axial compressor with casing treatment; part 1 – experiment. In: Proceedings of ASME Turbo Expo 2007: power for land, sea, and air, Bd 6: Turbo Expo 2007, parts A and B, paper GT2007-27581, Montreal, Canada, 14–17 May
Emmerich R, Kunte R, Hönen H, Niehuis R (2007b) Time resolved investigations of an axial compressor with casing treatment; part 2 – simulation. In: Proceedings of ASME Turbo Expo 2007: power for land, sea, and air, Bd 6: Turbo Expo 2007, parts A and B, paper GT2007-27582, Montreal, Canada, 14–17 May
Ivanov SK (1965) Axial blower. U. S. Patent No. 3189260
Miyake Y, Inaba T, Kato T (1987) Improvement of unstable characteristics of an axial flow fan by air-separator equipment. ASME J Fluids Eng 109(1):36–40
Hill SD, Elder RL, McKenzie AB (1998) Application of casing treatment to an industrial axialflow fan. Proc Inst Mech Eng A J Power Energy 212:225–233
Nishioka T, Kuroda S, Kozu T (2004) Improving stall margin by using an air-separator for a variable-pitch axial-flow fan. In: Proceedings of ASME Turbo Expo 2004: power for land, sea, and air, Bd 5: Turbo Expo 2004, parts A and B, paper GT2004-53663, Vienna, Austria, 14–17 June
Wang W, Chu W, Zhang H, Wu Y (2016) The effects on stability, performance and tip leakage flow of recirculating casing treatment in a subsonic axial flow compressor. In: Proceedings of ASME Turbo Expo 2016: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2016-56756, Seoul, South Korea, 13–17 June
Chen H, Li Y, Koley SS, Doeller N, Katz J (2017) An experimental study of stall suppression and associated changes to the flow structures in the tip region of an axial low speed fan rotor by axial casing grooves. In: Proceedings of ASME Turbo Expo 2017: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2017-65099, Charlotte, North Carolina, USA, 26–30 June
Streit JA, Guinet C, Heinichen F, Kau H-P (2012) Trading excessive stall margin for efficiency: an alternative approach to axial-slot casing treatments for transonic compressors. In: Conference paper, conference: 13th international symposium on unsteady aerodynamics, aeroacoustics and aeroelasticity of turbomachines, Tokyo, Japan
Suder KL, Hathaway MD, Thorp SA, Strazisar AJ, Bright MB (2001) Compressor stability enhancement using discrete tip injection. In: Proceedings of ASME Turbo Expo 2000: power for land, sea, and air, Bd 1: aircraft engine; marine; turbomachinery; microturbines and small turbomachinery, paper 2000-GT-650, Munich, Germany, 8–11 May
Khalegi H, Teixera JA, Tousi AM, Boroomand M (2008) Parametric study of injection angle effects on stability enhancement of transonic axial compressors. Journal of Propulsion and Power 24(5):1100–1107
Hathaway MD (2002) Self-recirculating casing treatment concept for enhanced compressor performance. In: Proceedings of self-recirculating casing treatment concept for enhanced compressor performance. Proceedings of ASME Turbo Expo 2002: power for land, sea, and air, Bd 5: Turbo Expo 2002, parts A and B, paper GT2002-30368, Amsterdam, The Netherlands, 3–6 June
Guinet C, Inzenhofer A, Gümmer V (2015) Influencing parameter of tip blowing interactions with rotor tip flow. In: Proceedings of ASME Turbo Expo 2015: turbine technical conference and exposition, Bd 2A: turbomachinery, paper GT2015-42039, Montreal, Quebec, Canada, 15–19 June
Hah C (2018) The inner workings of axial casing grooves in a one and a half stage. In: Proceedings of ASME Turbo Expo 2018: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2018-75040, Oslo, Norway, 11–15 June
Chen H, Li Y, Katz J (2018) On the interactions of a rotor blade tip flow with axial casing grooves in an axial compressor near the best efficiency point. In: Proceedings of ASME Turbo Expo 2018: turbomachinery technical conference and exposition, Bd 2A: turbomachinery, paper GT2018-77071, Oslo, Norway, 11–15 June
Author information
Authors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Fachmedien Wiesbaden GmbH, ein Teil von Springer Nature
About this chapter
Cite this chapter
Joos, F. (2020). Stabilisierung durch Wandkonturierung, „Endwall treatment“. In: Aerodynamik axialer Turbokompressoren. Springer Vieweg, Wiesbaden. https://doi.org/10.1007/978-3-658-28937-9_8
Download citation
DOI: https://doi.org/10.1007/978-3-658-28937-9_8
Published:
Publisher Name: Springer Vieweg, Wiesbaden
Print ISBN: 978-3-658-28936-2
Online ISBN: 978-3-658-28937-9
eBook Packages: Computer Science and Engineering (German Language)