Gas Turbine Engineering Handbook 2 Episode 11 doc

... F:/GTE/FINAL (26 -10 - 01) /FRONT MATTER.3D ± 1 ± [1 16 /16 ] 1. 11 .20 01 12 : 46PM Ga sTurbine Engineering Ha ndbook Second Edition G:/GTE/FINAL (26 -10 - 01) /CHAPTER 1. 3D ± 16 ± [1 57/57] 1. 11 .20 01 3:42PM Categories ... http://www.gulfpp.com 10 987654 3 21 Printed in the United States of America F:/GTE/FINAL (26 -10 - 01) /FRONT MATTER.3D ± 2 ± [1 16 /16 ] 1. 11 .2...

Ngày tải lên: 13/08/2014, 09:20

... (btu/lb-air) Efficiency % 20 00 1800 22 00 24 00 26 00 28 00 3000 1800 F° 9 82 C° 20 00 F° 1094 C° 22 00 F° 120 4 C° 24 00 F° 1316 C° 26 00 F° 1 427 C° 28 00 F° 1538 C° 3000 F° 1649 C° Pr = 5 7 9 11 13 15 20 30 40 17 Figure 2- 17. ... following: h 4   m a   m f h 4a   m s h 4s =  m a   m f   m s  2- 30 0 5 10 15 20 25 30 35 40 45 50 50.00 100.00 150.00 20...

Ngày tải lên: 13/08/2014, 09:20

... Figure 3- 3, the following relationships are 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 ... 117.44 20 1,6 92 459,967 661,659 Inter-stage compressor cooling 17.41 15.69 14.19 9,576 2. 5 1 43. 56 3, 7 43, 308 2, 291 ,36 5 6, 034 ,6 72 He...

Ngày tải lên: 13/08/2014, 09:20

... above Figure 4- 7. Fuel systems for gas turbines. 1 62 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 4. 3D ± 173 ± [ 141 ±177/37] 29 .10 .20 01 3:57PM Table 4 -2 continued 27 . ... lowest. Table 4- 1 shows how the maintenance cost would increase from natural gas to the heavy oils. 0 100 20 0 300 40 0 500 600 0 20 40 60 80 100 120 140...

Ngày tải lên: 13/08/2014, 09:20

... Compressors 23 1 //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 5. 3D ± 21 6 ± [178 21 8/41] 29 .10 .20 01 3 :57 PM Figure 5 -28 . Campbell diagram of tested impeller. 21 6 Gas Turbine Engineering Handbook ... 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 :57 PM i...

Ngày tải lên: 13/08/2014, 09:20

... Type,'' NACA TN - 26 04, 19 52. 27 4 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL ( 26 -10-01)/CHAPTER 6. 3D ± 23 5 ± [21 9 27 4/ 56] 29 .10 .20 01 3:59PM Figure 6- 18. Velocity profiles ... changes. Figure 6 -29 . Jet-wake flow distribution from an impeller. 24 6 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL ( 26 -10-01)/CHAP...

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 ... diagram. 29 8 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 7. 3D ± 3 02 ± [...

Ngày tải lên: 13/08/2014, 09:20

... (4 72  C), approximately 20  F (10  C) per year. The 1000 120 0 1400 1600 180 0 20 00 22 00 24 00 26 00 28 00 1950 1960 1970 1 980 1990 20 00 20 10 YEAR Firing Temperature F (°C)° U 500 RENE 77 IN 733 GTD111 GTD ... Blades,'' NASA, TM X -21 33, 1970. 3 68 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 9.3D ± 361 ± [337±369/3...

Ngày tải lên: 13/08/2014, 09:20

... 7 Â ± Â ± Â ± Â ± Â ± 0 .25 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 SS3 09 23 13 Â ± BAL Â ± Â ± Â ± Â ± Â ± Â ± ... G:/GTE/FINAL (26 -10-01)/CHAPTER 11.3D ± 421 ± [4 09 435 /27 ] 1.11 .20 01 3:51PM Other Oxides 2Mo3O 2 3 2 MoO 3 2W 3O 2 3 2WO 3 4V 5O 2 3 2V 2 O 5...

Ngày tải lên: 13/08/2014, 09:20

... 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

... (381mm) BEARING 12 INCH (305mm) BEARING SHAFT SPEED RPM ì 10 –3 024 6810 12 0 100 (75) 20 0 (149) 300 (22 4) 400 (29 9) Figure 13 -20 . Total power loss in thrust bearings. 494 Gas Turbine Engineering Handbook ... educted gas in the process. Figure 13- 32. Multiple combination segmented gas seal system. 5 12 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/F...

Ngày tải lên: 13/08/2014, 09:20

... signature to signature before overhaul. 5 82 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 16.3D ± 567 ± [558±583 /26 ] 29 .10 .20 01 4:05PM The second limitation of this ... high-pressure air into the spray nozzle manifold. 536 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 16.3D ± 568 ± [558±583 /26 ] 29...

Ngày tải lên: 13/08/2014, 09:20

... heat Figure 18 -2. Gear coupling (male teeth integral with the hub). 608 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 18.3D ± 613 ± [605±633 /29 ] 29 .10 .20 01 4:06PM Sludge ... the phase angle in an elliptic orbit. 5 92 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 18.3D ± 621 ± [605±633 /29 ] 29 .10...

Ngày tải lên: 13/08/2014, 09:20

... continuously. 0 20 40 60 80 100 120 0 2 4 6 8 10 12 14 Time in Minutes Percent of Parameters (%) Flow Power Firing Temperature Speed Figure 19-6. A typical shutdown curve for a gas turbine. 6 42 Gas Turbine Engineering Handbook ... with many composite 646 Gas Turbine Engineering Handbook G:/GTE/FINAL (26 -10-01)/CHAPTER 19.3D ± 6 42 ± [634±691/58] 1.11 .20 01...

Ngày tải lên: 13/08/2014, 09:20

... Temperature Turbine efficiency (%) 0 10 20 30 40 50 60 70 80 90 100 20 00 20 50 21 00 21 50 22 00 22 50 23 00 23 50 24 00 (1094 °C) (1149 C)° ( 120 4 C)° ( 126 0 C)° ( 128 8 C)° Figure 20 - 12. Gas turbine efficiency ... Design MW Turbine Type Efficiency at Design Output Point 1 2. 5 Steam 22 2 2.5 Steam 22 3 5.0 Steam 24 4 5.0 Steam 24 5 5.0 Steam 24 6 7.5 Ste...

Ngày tải lên: 13/08/2014, 09:20