Gas Turbine Engineering Handbook 2 Episode 7 docx

... 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 ± [ 2...

Ngày tải lên: 13/08/2014, 09:20

... #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 À10=30 15/95 68 10  F 15/110 Visc. CS @ 100  F 1.4 /2. 2 2. 48 /2. 67 2. 0/4.0 ... 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 ...

Ngày tải lên: 13/08/2014, 09:20

... 3. 32 0.39 10,891 0.5 135. 67 515 ,26 4 396 ,75 5 9 12, 019 Refrigeration inlet cooling 12. 77 11.51 2. 5 10,6 72 2.5 195 .74 605, 075 1, 379 ,901 1,984, 977 Ice storage cooling 12. 77 11.51 2. 5 10,6 72 1.5 1 17. 44 ... 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...

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 . Exhaust ... Typical protection system for a turbine. 170 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 4.3D ± 1 62 ± [141...

Ngày tải lên: 13/08/2014, 09:20

... 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 is apparent that a forcing frequency of 12, 000 rpm ... 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 ± [2...

Ngày tải lên: 13/08/2014, 09:20

... 20  F (10  C) per year. The 1000 120 0 1400 1600 1800 20 00 22 00 24 00 26 00 28 00 1950 1960 1 970 1980 1990 20 00 20 10 YEAR Firing Temperature F (°C)° U 500 RENE 77 IN 73 3 GTD111 GTD 111 DS GTD 111 SC GTD ... Blades,'' NASA, TM X -21 33, 1 970 . 368 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 9.3D ± 361 ± [3 37 369/33]...

Ngày tải lên: 13/08/2014, 09:20

... 28 10 BAL 1 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 SS309 23 13 Â ± BAL Â ± Â ± Â ± Â ± Â ± Â ± ... 1/1000 30,000 60,000 100,000 15,000 25 ,000 35,000 Nat. gas 1/10 75 00 42, 000 72 , 000 3 ,75 0 20 ,000 25 ,000 Distillate oil 1/1000 22 ,000...

Ngày tải lên: 13/08/2014, 09:20