Gas Turbine Engineering Handbook 2 Episode 10 docx

... 12. 8/14.5 12. 83 12/ 13 .2 14.75 10/ 12. 5 12. 40 12/ 13 .2 Carbon residue 10% bottoms .01/.1 .104 .03/.3 2/ 10 .3/3 Ash ppm 1/5 .001 0 /20 100 /1,000 36ppm 20 /20 0 Na  K ppm 01.5 0/1 1/350 2. 2/4.5 0/50 V ... #2 Oil #2 JP-4 Flash point  F 130/160 118 Â 22 0 150 /20 0 < RT 175 /26 5 186  F 198 50 /20 0 Pour point  F À50 À55 to 10 10= 30 15/95 68 10  F 15/ 110 Visc....

Ngày tải lên: 13/08/2014, 09:20

... Compressors 29 1 //INTEGRA/B&H/GTE/FINAL (26 -10- 01)/CHAPTER 7.3D ± 29 6 ± [27 5±318/44] 29 .10 .20 01 4:00PM and W 1 2  V z1 2 V z1 tan  2  2 7-18 W 2 2  V z2 2 V z2 tan  4  2 7-19 Therefore, H r  V z 2 2g c tan 2  2 À ... Axial-outflow stage velocity diagram. 29 8 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10- 01)...

Ngày tải lên: 13/08/2014, 09:20

... obtained: V 1 2  V 2  1  V 2 m 1 V 2 2  V 2  2  V 2 m 2 W 1 2 U 1 À V  1  2  V 2 m 1 W 2 2 U 2 À V  2  2  V 2 m 2 3 -21  Figure 3-3. Velocity triangles for an axial-flow compressor. 120 Gas ... fluid: 1 Work 2 h 1 À h 2  V 1 2 2g c À V 2 2 2g c  Z 1 À Z 2 3 -24  Combining the energy and momentum equations provides t...

Ngày tải lên: 13/08/2014, 09:20

... cost would increase from natural gas to the heavy oils. 0 100 20 0 300 400 500 600 0 20 40 60 80 100 120 140 160 180 20 0 22 0 24 0 GAS TURBINE- FRAME TYPE-RATED POWER (MW) 30 31 32 33 34 35 36 37 Efficiency Cost EFFICIENCY ... the aero-derivative turbines rated between 10 MW to 40 MW with an installed 0 20 0 400 600 800 100 0 120 0 024 6 810 12 GAS TURBINE- INDUSTRIA...

Ngày tải lên: 13/08/2014, 09:20

... Engine Group, Group Engineering Division, May 11, 19 72. ) 21 0 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10- 01)/CHAPTER 6.3D ± 23 0 ± [21 9 27 4/56] 29 .10 .20 01 3:59PM For nonprewhirl ... May 11, 19 72. ) 20 8 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10- 01)/CHAPTER 5.3D ± 21 2 ± [178 21 8/41] 29 .10 .20 01 3:57PM...

Ngày tải lên: 13/08/2014, 09:20

... loss. 366 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10- 01)/CHAPTER 9.3D ± 3 62 ± [337±369/33] 29 .10 .20 01 4:02PM Cooled -Turbine Aerodynamics The injection of coolant air in the turbine ... Blades,'' NASA, TM X -21 33, 1970. 368 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10- 01)/CHAPTER 9.3D ± 361 ± [337±369/33]...

Ngày tải lên: 13/08/2014, 09:20

... 0.01 Â ± N155 21 20 20 BAL 2. 5 3 Â ± Â ± Â ± Â ± 0 .20 Â ± Â ± GTD -22 2 22 .5 BAL 19 Â ± 2. 0 2. 3 1 .2 0.8 Â ± 0 .10 0.008 1.00 Â ± Combustors SS309 23 13 Â ± BAL Â ± Â ± Â ± Â ± Â ± Â ± 0 .10 Â ± Â ± HAST X 22 ... 30,000 60,000 100 ,000 15,000 25 ,000 35,000 Nat. gas 1 /10 7500 42, 000 72, 000 3,750 20 ,000 25 ,000 Distillate oil 1 /100 0 22 ,000 45,000 72, 000 11 ,25...

Ngày tải lên: 13/08/2014, 09:20