메뉴 건너뛰기




Volumn 134, Issue 3, 2012, Pages

Recent advances in turbine Heat Transfer-with a view of transition to coal-gas based systems

Author keywords

endwall; film cooling; heat transfer coefficient; leading edge; main body; tip turn; trailing edge

Indexed keywords

END-WALL; FILM COOLING; LEADING EDGE; MAIN BODY; TIP TURN; TRAILING EDGES;

EID: 84856098387     PISSN: 00221481     EISSN: 15288943     Source Type: Journal    
DOI: 10.1115/1.4005148     Document Type: Article
Times cited : (22)

References (61)
  • 1
    • 85025203077 scopus 로고    scopus 로고
    • Aerothermal challenges in syngas, hydrogen-fired and oxy-fuel turbines: Part I-gas side heat transfer
    • Chyu, M. K., Siw, S., Mazzotta, D., Karaivanov, V., and Alvin, M. A., 2009, " Aerothermal Challenges in Syngas, Hydrogen-Fired and Oxy-Fuel Turbines: Part I-Gas Side Heat Transfer.," ASME Trans. J. Therm. Sci. Eng. Appl., 1, p. 011002. 10.1115/1.3159479
    • (2009) ASME Trans. J. Therm. Sci. Eng. Appl. , vol.1 , pp. 011002
    • Chyu, M.K.1    Siw, S.2    Mazzotta, D.3    Karaivanov, V.4    Alvin, M.A.5
  • 2
    • 84922797706 scopus 로고    scopus 로고
    • Aerothermal challenges in syngas, hydrogen-fired and oxy-fuel turbines: Part II-effects of internal heat transfer
    • Chyu, M. K., Siw, S., Karaivanov, V., and Alvin, M. A., 2009, " Aerothermal Challenges in Syngas, Hydrogen-Fired and Oxy-Fuel Turbines: Part II-Effects of Internal Heat Transfer.," ASME Trans. J. Therm. Sci. Eng. Appl., 1, p. 011003. 10.1115/1.3159480
    • (2009) ASME Trans. J. Therm. Sci. Eng. Appl. , vol.1 , pp. 011003
    • Chyu, M.K.1    Siw, S.2    Karaivanov, V.3    Alvin, M.A.4
  • 4
    • 85014222310 scopus 로고    scopus 로고
    • 3rd ed., Gulf Professional Publishing, Houston, TX
    • Boyce, M. P., 2006, Gas Turbine Engineering Handbook, 3rd ed., Gulf Professional Publishing, Houston, TX, pp. 47-48.
    • (2006) Gas Turbine Engineering Handbook , pp. 47-48
    • Boyce, M.P.1
  • 5
    • 0027610165 scopus 로고
    • Progress towards understanding and predicting heat transfer in the turbine gas path
    • DOI 10.1016/0142-727X(93)90019-J
    • Simoneau, R. J., and Simon, F. F., 1993, " Progress Towards Understanding and Predicting Heat Transfer in the Turbine Gas Path.," Int. J. Heat Fluid Flow, 14 (2), pp. 106-128. 10.1016/0142-727X(93)90019-J (Pubitemid 23683372)
    • (1993) International Journal of Heat and Fluid Flow , vol.14 , Issue.2 , pp. 106-128
    • Simoneau Robert, J.1    Simon Frederick, F.2
  • 8
    • 47949098553 scopus 로고    scopus 로고
    • Analytical modeling of turbine cascade leading edge heat transfer using skin friction and pressure measurements
    • Holley, B. M., and Langston, L. S., 2008, " Analytical Modeling of Turbine Cascade Leading Edge Heat Transfer Using Skin Friction and Pressure Measurements.," ASME J. Turbomach., 130, p. 021001. 10.1115/1.2812328
    • (2008) ASME J. Turbomach. , vol.130 , pp. 021001
    • Holley, B.M.1    Langston, L.S.2
  • 9
    • 0028257740 scopus 로고
    • Interactions between Embedded Vortices and Injectant from Film Cooling Holes with Compound Angle Orientations in a Turbulent Boundary Layer
    • 10.1115/1.2928281
    • Ligrani, P. M., and Mitchell, S. W., 1994, " Interactions Between Embedded Vortices and Injectant From Film Cooling Holes With Compound Angle Orientations in a Turbulent Boundary Layer.," ASME J. Turbomach., 116 (1), pp. 80-91. 10.1115/1.2928281
    • (1994) ASME J. Turbomach. , vol.116 , Issue.1 , pp. 80-91
    • Ligrani, P.M.1    Mitchell, S.W.2
  • 10
    • 4243193913 scopus 로고    scopus 로고
    • Film cooling with compound angle holes: Adiabatic effectiveness
    • 10.1115/1.2840938
    • Schmidt, D., Sen, B., and Bogard, D., 1996, " Film Cooling With Compound Angle Holes: Adiabatic Effectiveness.," ASME J. Turbomach., 118, pp. 807-813. 10.1115/1.2840938
    • (1996) ASME J. Turbomach. , vol.118 , pp. 807-813
    • Schmidt, D.1    Sen, B.2    Bogard, D.3
  • 11
    • 0030446933 scopus 로고    scopus 로고
    • Film cooling with compound angle holes: Heat transfer
    • 10.1115/1.2840937
    • Sen, B., Schmidt, D., and Bogard, D., 1996, " Film Cooling With Compound Angle Holes: Heat Transfer.," ASME J. Turbomach., 118, pp. 800-806. 10.1115/1.2840937
    • (1996) ASME J. Turbomach. , vol.118 , pp. 800-806
    • Sen, B.1    Schmidt, D.2    Bogard, D.3
  • 12
    • 79952025306 scopus 로고    scopus 로고
    • Turbine blade film cooling using PSP techniques
    • Han, J. C., and Rallabandi, A. P., 2010, " Turbine Blade Film Cooling Using PSP Techniques.," Front. Heat Mass Transfer, 1 (1), pp. 1-21.
    • (2010) Front. Heat Mass Transfer , vol.1 , Issue.1 , pp. 1-21
    • Han, J.C.1    Rallabandi, A.P.2
  • 13
    • 33645773202 scopus 로고    scopus 로고
    • Gas turbine film cooling
    • 10.2514/1.18034
    • Bogard, D. G., and Thole, K. A., 2006, " Gas Turbine Film Cooling.," J. Propul. Power, 22 (2), pp. 249-270. 10.2514/1.18034
    • (2006) J. Propul. Power , vol.22 , Issue.2 , pp. 249-270
    • Bogard, D.G.1    Thole, K.A.2
  • 14
    • 0016061470 scopus 로고
    • Effects of hole geometry and density on three-dimensional film cooling
    • 10.1016/0017-9310(74)90007-6
    • Goldstein, R. J., Eckert, E. R. G., and Burggraf, F., 1974, " Effects of Hole Geometry and Density on Three-Dimensional Film Cooling.," Int. J. Heat Mass Transfer, 17, pp. 595-607. 10.1016/0017-9310(74)90007-6
    • (1974) Int. J. Heat Mass Transfer , vol.17 , pp. 595-607
    • Goldstein, R.J.1    Eckert, E.R.G.2    Burggraf, F.3
  • 15
    • 18844461281 scopus 로고    scopus 로고
    • A review of shaped hole turbine film-cooling technology
    • DOI 10.1115/1.1860562
    • Bunker, R. S., 2005, " A Review of Turbine Shaped Film Cooling Technology.," J. Heat Transfer, 127, pp. 441-453. 10.1115/1.1860562 (Pubitemid 40687145)
    • (2005) Journal of Heat Transfer , vol.127 , Issue.4 , pp. 441-453
    • Bunker, R.S.1
  • 18
    • 0025460721 scopus 로고
    • Local heat transfer in internally cooled turbine airfoil leading edge regions. Part I. Impingement cooling without film coolant extraction
    • Bunker, R. S., and Metzger, D. E., 1990, " Local Heat Transfer in Internal Cooled Turbine Airfoil Leading Edge Regions: Part I-Impingement Cooling Without Film Coolant Extraction.," ASME J. Turbomach., 112 (3), pp. 451-458. 10.1115/1.2927680 (Pubitemid 20711088)
    • (1990) Journal of Turbomachinery , vol.112 , Issue.3 , pp. 451-458
    • Bunker, R.S.1    Metzger, D.E.2
  • 19
    • 0034953282 scopus 로고    scopus 로고
    • Jet-impingement heat transfer in gas turbine systems
    • Han, B., and Goldstein, R. J., 2001, " Jet-Impingement Heat Transfer in Gas Turbine Systems.," Ann. N.Y. Acad. Sci., 934 (1), pp. 147-161. 10.1111/j.1749-6632.2001.tb05849.x (Pubitemid 32612813)
    • (2001) Annals of the New York Academy of Sciences , vol.934 , pp. 147-161
    • Han, B.1    Goldstein, R.J.2
  • 22
    • 33745235272 scopus 로고    scopus 로고
    • Heat transfer of impinging jet-array over convex-dimpled surface
    • DOI 10.1016/j.ijheatmasstransfer.2006.02.030, PII S0017931006001323
    • Chang, S. W., Jan, Y. J., and Chang, S. F., 2006, " Heat Transfer of Impinging Jet-Array Over Convex-Dimpled Surface.," Int. J. Heat Mass Transfer, 49 (17-18), pp. 3045-3059. 10.1016/j.ijheatmasstransfer.2006.02.030 (Pubitemid 43922365)
    • (2006) International Journal of Heat and Mass Transfer , vol.49 , Issue.17-18 , pp. 3045-3059
    • Chang, S.W.1    Jan, Y.J.2    Chang, S.F.3
  • 24
    • 77649258410 scopus 로고    scopus 로고
    • Enhanced internal cooling of turbine blades and vanes
    • U.S. Department of Energy, Office of Fossil Energy, NETL
    • Han, J. C., and Wright, L. M., 2006, " Enhanced Internal Cooling of Turbine Blades and Vanes.," The Gas Turbine Handbook, U.S. Department of Energy, Office of Fossil Energy, NETL, pp. 321-354.
    • (2006) The Gas Turbine Handbook , pp. 321-354
    • Han, J.C.1    Wright, L.M.2
  • 25
    • 0034957513 scopus 로고    scopus 로고
    • Recent developments in turbine blade internal cooling
    • Han, J. C., and Dutta, S., 2001, " Recent Developments in Turbine Blade Internal Cooling.," Ann. N.Y. Acad. Sci., 934 (1), pp. 162-178. 10.1111/j.1749-6632.2001.tb05850.x (Pubitemid 32612814)
    • (2001) Annals of the New York Academy of Sciences , vol.934 , pp. 162-178
    • Han, J.-C.1    Dutta, S.2
  • 27
    • 84856086067 scopus 로고    scopus 로고
    • European Patent Specification, EP 1,617,043 B1
    • Lafleur, R. S., 2008, European Patent Specification, EP 1,617,043 B1.
    • (2008)
    • Lafleur, R.S.1
  • 33
    • 33645775533 scopus 로고    scopus 로고
    • Trailing-edge cooling for gas turbines
    • 10.2514/1.20898
    • Cunha, F. J., and Chyu, M. K., 2006, " Trailing-Edge Cooling for Gas Turbines.," J. Propul. Power, 22 (2), pp. 286-300. 10.2514/1.20898
    • (2006) J. Propul. Power , vol.22 , Issue.2 , pp. 286-300
    • Cunha, F.J.1    Chyu, M.K.2
  • 36
    • 7644220314 scopus 로고    scopus 로고
    • Experimental and Numerical Investigation of Trailing Edge Film Cooling by Circular Coolant Wall Jets Ejected from a Slot with Internal Rib Arrays
    • 10.1115/1.1645531
    • Martini, P., and Schulz, A., 2004, " Experimental and Numerical Investigation of Trailing Edge Film Cooling by Circular Coolant Wall Jets Ejected from a Slot With Internal Rib Arrays.," ASME J. Turbomach., 126 (2), pp. 229-236. 10.1115/1.1645531
    • (2004) ASME J. Turbomach. , vol.126 , Issue.2 , pp. 229-236
    • Martini, P.1    Schulz, A.2
  • 39
    • 0019074240 scopus 로고
    • Crossflows in a Turbine Cascade Passage
    • 10.1115/1.3230352
    • Langston, L. S., 1980, " Crossflows in a Turbine Cascade Passage.," ASME J. Eng. Power, 102, pp. 866-874. 10.1115/1.3230352
    • (1980) ASME J. Eng. Power , vol.102 , pp. 866-874
    • Langston, L.S.1
  • 40
    • 0023324596 scopus 로고
    • Predictions of endwall losses and secondary flows in axial flow turbine cascades
    • Sharma, O. P. and Butler, T. L., 1987, " Predictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades.," ASME J. Turbomach., 109, pp. 229-236. 10.1115/1.3262089 (Pubitemid 17549890)
    • (1987) Journal of Turbomachinery , vol.109 , Issue.2 , pp. 229-236
    • Sharma, O.P.1    Butler, T.L.2
  • 41
    • 33645781565 scopus 로고    scopus 로고
    • Turbine endwall aerodynamics and heat transfer
    • 10.2514/1.16344
    • Simon, T. W., and Piggush, J. D., 2006, " Turbine Endwall Aerodynamics and Heat Transfer.," J. Propul. Power, 22 (2), pp. 301-312. 10.2514/1.16344
    • (2006) J. Propul. Power , vol.22 , Issue.2 , pp. 301-312
    • Simon, T.W.1    Piggush, J.D.2
  • 43
    • 0023436995 scopus 로고
    • Film Cooling on a Turbine Blade with Injection through Two Rows of Holes in the Near-Endwall Region
    • 10.1115/1.3262152
    • Goldstein, R. J., and Chen, P. H., 1987, " Film Cooling on a Turbine Blade With Injection through Two Rows of Holes in the Near-Endwall Region.," ASME J. Turbomach., 109, pp. 588-593. 10.1115/1.3262152
    • (1987) ASME J. Turbomach. , vol.109 , pp. 588-593
    • Goldstein, R.J.1    Chen, P.H.2
  • 45
  • 46
    • 0032125003 scopus 로고    scopus 로고
    • Influence of gap leakage downstream of the injection holes on film cooling performance
    • Yu, Y., and Chyu, M. K., 1998, " Influence of a Leaking Gap Downstream of the Injection Holes on Film Cooling Performance.," ASME J. Turbomach., 120, pp. 541-548. (Pubitemid 28504435)
    • (1998) Journal of Turbomachinery , vol.120 , Issue.3 , pp. 541-548
    • Yu, Y.1    Chyu, M.K.2
  • 47
    • 0034953626 scopus 로고    scopus 로고
    • Heat transfer near turbine nozzle endwall
    • Chyu, M. K., 2001, " Heat Transfer Near Turbine Nozzle Endwall.," Ann. N.Y. Acad. Sci., 934, pp. 27-36. 10.1111/j.1749-6632.2001. tb05840.x (Pubitemid 32618708)
    • (2001) Annals of the New York Academy of Sciences , vol.934 , pp. 27-36
    • Chyu, M.K.1
  • 51
    • 0019600102 scopus 로고
    • Experimental Investigation of Endwall Profiling in a Turbine Vane Cascade
    • 10.2514/3.51032
    • Kopper, F. C., Milano, R., and Vanco, M., 1981, " Experimental Investigation of Endwall Profiling in a Turbine Vane Cascade.," AIAA J., 19 (8), pp. 1020-1040. 10.2514/3.51032
    • (1981) AIAA J. , vol.19 , Issue.8 , pp. 1020-1040
    • Kopper, F.C.1    Milano, R.2    Vanco, M.3
  • 56
    • 85003411202 scopus 로고
    • Heat transfer in shrouded rectangular cavities
    • 10.2514/3.35
    • Chyu, M. K., Metzger, D. E., and Hwan, C. L., 1987, " Heat Transfer in Shrouded Rectangular Cavities.," AIAA J. Thermophys. Heat Transfer, 1, pp. 247-252. 10.2514/3.35
    • (1987) AIAA J. Thermophys. Heat Transfer , vol.1 , pp. 247-252
    • Chyu, M.K.1    Metzger, D.E.2    Hwan, C.L.3
  • 57
    • 0024607015 scopus 로고
    • Cavity Heat Transfer on a Transverse Grooved Wall in a Narrow Flow Channel
    • 10.1115/1.3250661
    • Metzger, D. E., Bunker, R. S., and Chyu, M. K., 1989, " Cavity Heat Transfer on a Transverse Grooved Wall in a Narrow Flow Channel.," ASME J. Heat Transfer, 111, pp. 73-79. 10.1115/1.3250661
    • (1989) ASME J. Heat Transfer , vol.111 , pp. 73-79
    • Metzger, D.E.1    Bunker, R.S.2    Chyu, M.K.3
  • 58
    • 0029136996 scopus 로고
    • Heat transfer and effectiveness of film cooled turbine blade tip models
    • 21. 10.1115/1.2835630
    • Kim, Y. W., and Metzger, D. E., 1995, " Heat Transfer and Effectiveness of Film Cooled Turbine Blade Tip Models.," ASME J. Turbomach., 117, pp. 12 21. 10.1115/1.2835630
    • (1995) ASME J. Turbomach. , vol.117 , pp. 12
    • Kim, Y.W.1    Metzger, D.E.2
  • 59
    • 0034963175 scopus 로고    scopus 로고
    • A review of turbine blade tip heat transfer
    • Bunker, R. S., 2001, " A Review of Turbine Blade Tip Heat Transfer.," Ann. N.Y. Acad. Sci., 934, pp. 64-79. 10.1111/j.1749-6632.2001. tb05843.x (Pubitemid 32612807)
    • (2001) Annals of the New York Academy of Sciences , vol.934 , pp. 64-79
    • Bunker, R.S.1
  • 60
    • 33645772973 scopus 로고    scopus 로고
    • Axial turbine blade tips: Function, design, and durability
    • 10.2514/1.11818
    • Bunker, R. S., 2006, " Axial Turbine Blade Tips: Function, Design, and Durability.," J. Propul. Power, 22 (2), pp. 271-287. 10.2514/1.11818
    • (2006) J. Propul. Power , vol.22 , Issue.2 , pp. 271-287
    • Bunker, R.S.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.