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LIST OF FIGURES Figure 1. GE-Alstom (former Brown Boveri) heavy duty power generation gas turbine GT13E2 with gross output of 203 MW; Reprinted from GE Power [2]........................................................................................................................1 Figure 2. A three-stage high pressure research turbine at TPFL. The blades are cylindrical with tip shroud to reduce the tip leakage losses; Reprinted from Schobeiri [1]. ......................................................................................................2 Figure 3. Siemens SGT-800 power generation gas turbine (57.0 MW); Reprinted from Siemens [3]. ...............................................................................................4 Figure 4. Rolls Royce Trent 1000 aircraft engine. Three-spool, high-bypass ratio gas turbine, designed and optimized for the Boeing 787 Dreamliner; Reprinted from Rolls Royce [4]. .........................................................................................4 Figure 5. Efficiency comparison between a conventional (blue curve) and a reheat (green curve) gas turbine; Reprinted from Schobeiri [5]....................................6 Figure 6. Brown Boveri (GE-Alstom) GT 24/26 with two combustion stages and a reheat turbine stage; Reprinted from GE Power [2]. ..........................................6 Figure 7. Compressed air energy storage facility, Huntorf, Germany: (1) LP-Gear, HP-Compressor train, (2) electric motor/generator, (3) gas turbine with two combustion chambers and two multi-stage turbines, (4) air storage; Reprinted from Schobeiri [12]..........................................................................10 Figure 8. CAES gas turbine engine; Reprinted from Schobeiri [12]. ..............................11 Figure 9. Process comparison for (a) baseline-conventional GT, (b) GT-24, and (c) UHEGT (four stages); detailed processes are: compression 1–2, combustion 2–3, 4–5, 6–7, and 8–9, expansion: 3–4, 5–6, 7–8, and 9–10; Reprinted from Schobeiri [8].............................................................................................14 Figure 10. (a) Thermal efficiency and (b) specific work comparison of baseline GT, GT-24, and different UHEGT configurations; Reprinted from Ref. [15]. .......17 Figure 11. Technology change from conventional GT to more advanced GT24/26 and the most advanced engine with an integrated UHEGT technology: (a) conventional technology, (b) New technology, and (c) UHEGT technology; Reprinted from Ref. [15]. .................................................................................18 xivPDF Image | DEVELOPMENT OF AN ULTRA-HIGH EFFICIENCY GAS TURBINE ENGINE (UHEGT
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