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Recent Advances In Energy Materials For Hot Sections Of Modern Gas-Turbine Engines

Authors: Zainul Huda;

Recent Advances In Energy Materials For Hot Sections Of Modern Gas-Turbine Engines

Abstract

{"references": ["Z. Huda, Metallurgical Failure Analysis for a Blade Failed in a Gas-\nTurbine Engine of a Power Plant; Materials and Design, 30 (2009) pp 3121 - 3125", "Z. Huda, \"Development of Design Principles for a Creep-Limited Alloy\nfor Turbine Blades' Journal of Materials Engineering & Performance;\nASM International, 4 (1) (1995) pp. 48-53", "Z. Huda, \"Development of Heat Treatment Process for a P/M Superalloy\nfor Turbine Blades\", Materials and Design, 28 (5) (2007) pp. 1664 -1667", "R. C. Reed, The Superalloys: Fundamentals and Applications:\nCambridge University Press, (2006)", "W.-D. Cao, In: E.A. Loria, Editor, Superalloys 718, 625, 706 and Derivatives, The Minerals, Metals & Materials Society, Warrendale\n(2005), pp. 165-177", "U. Martin, M. Jerenz, U. M\u251c\u255dhle, and H. Oettel, Microstructure and\nModeling of the High Temperature Deformation Behavior of TBCCoated\nSuperalloys, Materials Science and Engineering A, 319-321 (2001) pp. 388-392", "I. Gurrappa and R.A. Sambasiva, Thermal Barrier Coatings for\nEnhanced Efficiency of Gas Turbine Engines, Surface & Coatings\nTechnology 201 (2006) pp. 3016 - 3029", "D. St\u00f6ver, C. Funke, Directions of the Development of Thermal Barrier\nCoatings in Energy Applications, J. Materials Processing Technology,\n92-93 (1999) pp.195-202", "M.E. Miller and W.L. Chambers: In Superalloys II; Editors: C.T. Sims,\nN.S. Stoloff and W.C. Hagel; John Wiley & Sons, 1987\n[10] D.M. Todd, \"GE Combined Cycle Experience\": 33rd GD Turbine Stateof-\nthe-Art Tech Seminar, Paper No. GER-3585A, USA, (1989)\n[11] G.A. Zickler, R. Schnitzer, R. Radis, R. Hochfellner, R. Schweins, M.\nStockinger, and H. Leitner, \"Microstructure and mechanical properties\nof the superalloy ATI Allvac\u00ae 718Plus\u2122\", Materials Science & Engineering A 523 (1-2) (2009) pp. 295-303\n[12] S.A. Sajjadi and S. Nategh, A high-temperature deformation mechanism\nmap for the high performance Ni-base superalooy: GTD-111; Materials.\nScience &. Engineering A, 307 (1-2) (2001), pp. 158-164\n[13] S.A.Sajjadi, S. Nategh, and R.I.L. Guthrie, Study of microstructure and\nmechanical properties of high-performance Ni-base superalloy: GTD-\n111; Mater. Sci. Eng. A 325 (2002), p. 484-489\n[14] S.A. Sajjadi, S.M. Zebarjad, R.I.L Guthrie, and M. Isac; Microstructure\nevolution of high-performance Ni-base superalloy GTD-111 with heat\ntreatment parameters; J. Materials Processing Technology, 175 (1-3)\n(2006) pp. 376-381"]}

This presentation reviews recent advances in superalloys and thermal barrier coating (TBC) for application in hot sections of energy-efficient gas-turbine engines. It has been reviewed that in the modern combined-cycle gas turbines (CCGT) applying single-crystal energy materials (SC superalloys) and thermal barrier coatings (TBC), and – in one design – closed-loop steam cooling, thermal efficiency can reach more than 60%. These technological advancements contribute to profitable and clean power generation with reduced emission. Alternatively, the use of advanced superalloys (e.g. GTD-111 superalloy, Allvac 718Plus superalloy) and advanced thermal barrier coatings (TBC) in modern gas-turbines has been shown to yield higher energy-efficiency in power generation.

Keywords

superalloy, gas turbine engines, Energy materials, thermal barrier coating

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This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
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