Gas Turbine Engineering Handbook 2 Episode 17 ppt
Gas Turbine Engineering Handbook 2 Episode 17 ppt
... 301 Â ±3 Inducers, 23 6 Â ±7 camberlines, 23 6, 27 8 Â ±9 inlet (impeller eye), 23 0 systems, 22 5 Inlet guide vanes, 22 9 Â ± 32 nonprewhirl, 23 0 prewhirl, 22 9 Â ± 32 types, 22 9 Â ± 32 Influence coefficient method, ... 427 forgings and nondestructive testing, 427 Â ±9 gas turbine, 422 Â ±7 turbine wheel alloys, 425 Â ±7 gas turbine materials, 422 Â ±7 general met...
Ngày tải lên: 13/08/2014, 09:20
Gas Turbine Engineering Handbook 2 Episode 1 pptx
... 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
Gas Turbine Engineering Handbook 2 Episode 12 ppt
... 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
Gas Turbine Engineering Handbook 2 Episode 13 ppt
... shown Figure 17- 7. Typical probe positions and 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 .20 01 ... prealignment survey, (2) cold alignment, and (3) the hot alignment check. 624 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPT...
Ngày tải lên: 13/08/2014, 09:20
Gas Turbine Engineering Handbook 2 Episode 2 potx
... % 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 0.00 25 0.00 300.00...
Ngày tải lên: 13/08/2014, 09:20
Gas Turbine Engineering Handbook 2 Episode 3 pot
... 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
Gas Turbine Engineering Handbook 2 Episode 4 pot
... 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 . ... 4-10. Typical protection system for a turbine. 170 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 4.3D ± 1 62 ± [141 177 /37] 29...
Ngày tải lên: 13/08/2014, 09:20
Gas Turbine Engineering Handbook 2 Episode 5 pps
... 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 ... onset. 2. Axisymmetric 2. Eliminates instability. 3. Damping Introduce damping. 20 4 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER...
Ngày tải lên: 13/08/2014, 09:20
Gas Turbine Engineering Handbook 2 Episode 6 pps
... 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
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 ... 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