Advanced Gas Turbine Cycles Episode 1 ppt

... 10 3 10 5 10 7 10 7 10 9 10 9 10 9 11 0 11 1 11 2 11 4 11 6 11 7 11 8 12 2 12 3 12 6 12 8 12 9 13 1 13 1 13 2 13 2 13 3 13 3 13 5 13 5 13 6 13 6 13 6 13 9 14 0 14 0 14 1 Partial oxidation 14 3 ... Figs. 4 .1, 4.2, 4.3, 4.4, 4.5, 4.6, 4.7, 4 .11 , 4 .12 ,5.4,5.6,5.9,5 .10 ,5 .11 ,6 .1, 6.8,6.9,6 .10 ,6 .12 ,6 .14 ,6 .18 ,6 .19 ,6.20,7.4,7.7,7 .11 , 8 .1, 8...

Ngày tải lên: 13/08/2014, 15:21

... Basic gas turbine cycles 39 brackets [A] in Eq. (3.25) is linear with x, passing through the x, y points [l, 01; [ 1, (1 - E)]; [(p + 1) /2 ,1/ 2], where l = 1 - [(p - 1) (1 ... Similarly, the pressure loss 44 Advanced gas turbine cycles 55 50 48 5 tiu 2 $35 Ym 4 Y Y 2 25 z 20 15 10 800 800 looo 12 00 14 00 16 00 18 00 Moo 2...

Ngày tải lên: 13/08/2014, 15:21

... Calculating gas turbine performance, Engineering 18 1, 3 61 -367. 15 1 Horlock, J.H. (19 98). The evaporative gas turbine, ASME J. Engng Gas Turbines Power 12 0.336-343. [ 61 El-Masri, M.A. (19 88). ... Polsky, M. (19 %), The cascaded humidified advanced turbine (CHAT), ASME J. Engng Gas Turbines Power 11 8,565-5 71. [12 ] van Liere, J. (20 01) , Th...

Ngày tải lên: 13/08/2014, 15:21

... intercooled advanced gas turbine cycles is done. II List Of Contents 1. Introduction 1 2. Description of the LMS100 and its features 3 2 .1 Description of the thermodynamic process 4 2 .1. 1 ... simple gas turbine cycle 4 2 .1. 2 Influence of the cycle parameters on its efficiency and other properties 7 2 .1. 3 Improvements of the gas turbine simple cycle 9...

Ngày tải lên: 08/08/2014, 11:21

... k cc =1, k ic =1, η pt =1, η pc =1) 31 Figure 15 : Thermal efficiency (π T , n, θ=5.74, k cc =1, k ic =1, η pt =1, η pc =1) 31 Figure 16 : Dimensionless specific work (π T , n, θ=4.0, k cc =1. 12, ... Figure 12 : Dimensionless specific work (π T , n, θ=5.74, k cc =1, k ic =1, η pt =1, η pc =1) 30 Figure 13 : Thermal efficiency (π T , n, θ=4.00, k cc =1, k ic =1, η...

Ngày tải lên: 08/08/2014, 11:21

... Fig. 1. 9), ffA > ffB (a is less than unity) and 5 < 1 so that the thermal efficiency is 7 q= 1 - - < qcm = 1 - 7, 5 7 T q= 1 - = 1 - G. (1. 19) 1. 5. Modifications ... Combustion 1 Reactants { ~~~’-~~ chamber I Exhaust gases Generator (products) IW ‘ Compressor Turbine I 1- - - - - - - - - - - - - -1 Fig. 1...

Ngày tải lên: 13/08/2014, 15:21

... vjB = 1, from Eqs. (2.33) and (1. 17) (2.34) Chapter 3. Basic gas turbine cycles 31 - -[CHwR T3/Tl=4 CARNOT T-l= 4 [CHTXIR T -1 = 6.25 CARNOT T3/T1 = 6.25 1 1.5 2 2.5 ... Chapter 3. Basic gas turbine cycles 35 The specific heat supplied is q = cp(T3 - T2) = CpT1K8 - 1) - (x - 1) /77cl, 4 = cPr3 - ~ ~1= C,Tw - 1) - (XC - 1...

Ngày tải lên: 13/08/2014, 15:21

... large turbine cooling flows, ASME J. Engng Gas Turbines Power 12 3(3), 487-494. 3 61 -3 61. 583-592. machinery 12 4, 207- 213 . also p. 17 81) . ASME J. Engng Power Gas Turbines 10 9,228-235. ... with pressure ratio as a parameter. 68 Advanced gas turbine cycles 45 30 Y 0 20 15 + UNCOOLED lo00 12 M) 14 00 16 00 18 00 XI00 12 00 2400 2600 2800...

Ngày tải lên: 13/08/2014, 15:21

... Part 11 Model for expansion in cooled turbines, ASME J. Engng Power Gas Turbines 10 8, 15 1 - 15 9. 18 1 El-Masri, M.A. (19 88). GASCAN-an interactive code for thermal analysis of gas turbine ... Power Gas Turbines 1 10 ,2 01 -209. ( 91 El-Man, M.A. (19 87a). Exergy analysis of combined cycles: Part 1 Air-cooled Brayton-cycle gas turbines, ASME J. Engng Power...

Ngày tải lên: 13/08/2014, 15:21

... Engng Gas Turbines [I 61 ABB Power Generation (l997), The GT24/26 gas turbines, ABB Brochure PGT 218 6. Boveri Review 47,783-799. Turbines 10 7(4), 856-860. Gas Turbines Power 11 3(2), 19 0 -19 5. ... Vol. 1. achieve greater than 60% efficiency, ASME J. Engng Gas Turbines Power 11 7 (1) , 734-7 41. Power, 10 2, 1, Part I, 35- 41, Part II,42-49; 13 , 2, 19...

Ngày tải lên: 13/08/2014, 15:21