Gas Turbine Engineering Handbook 2 Episode 2 potx

... (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

... 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] 29 .10 .20 01 4:02PM Steam-Cooled Turbine Blades This ... blade. 356 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 9.3D ± 3 42 ± [337±369/33] 29 .10 .20 01 4:02PM The value of the wor...

Ngày tải lên: 13/08/2014, 09:20

... required 411 G:/GTE/FINAL (26 -10-01)/CHAPTER 11.3D ± 421 ± [409±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 The Ni-base alloy surface is exposed to an oxidizing gas, ... 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...

Ngày tải lên: 13/08/2014, 09:20

... overhauls. 0 5 10 15 20 25 30 35 40 45 50 40.00 60.00 80.00 100.00 120 .00 140.00 160.00 180.00 20 0.00 22 0.00 24 0.00 26 0.00 Net Output Work (btu/lb-air) Efficiency % 1800 20 00 22 00 24 00 26 00 28 00 3000 3000 ... F° 1649 C° 28 00 F° 1538 C° 26 00 F° 1 427 C° 24 00 F° 1316 C° 22 00°F 120 4 C° 20 00 F° 1094 C° 1800 F° 9 82 C° Pr =5 7 9 11 13 40 30 15 20 17 Figure 1-6....

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

... 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 diffuser 28 . ... 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...

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 ± [21 9...

Ngày tải lên: 13/08/2014, 09:20

... Mixed-Flow 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 ... as seen in Figure 6- 32. This loss is the same for a given 25 0 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 6.3D ± 24 7 ± [...

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 ...  4  2 7-19 Therefore, H r  V z 2 2g c tan 2  2 À tan 2  4  Thus, the reaction of the stage can be written R...

Ngày tải lên: 13/08/2014, 09:20

... 0 Â 20 .1/80 Residual 0 Â ±1 0 Â 20 0 Â ±100 5/400 Crude 0 Â ±1 0 Â 20 0 Â ± 122 .1/80 4 42 Gas Turbine Engineering Handbook G:/GTE/FINAL (26 -10-01)/CHAPTER 12. 3D ± 460 ± [436±466/31] 1.11 .20 01 ... #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...

Ngày tải lên: 13/08/2014, 09:20