Gas Turbine Engineering Handbook 2 Episode 2 potx

... (btu/lb-air)Efficiency % 20 001800 22 00 24 00 26 00 28 0030001800 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 = 579111315 20 304017Figure 2- 17. ... following:h4mamfh4amsh4s=mamfms 2- 30051015 20 25 303540455050.00 100.00 150.00 20 0.00 25 0.00 300.00 350.00 400.00 450.00Net Output Work (btu/lb-air)Thermal Efficiency % 20 001800 22 00 24 00 26 00 28 0030001800 F°9 82 C° 20 00 F°1094 ... compressor efficiency of 87% and a turbine efficiency of 92% . 62 Gas Turbine Engineering Handbook G:/GTE/FINAL (26 -10-01)/CHAPTER 2. 3D ± 84 ± [58±111/54] 1.11 .20 01 3:47PMat 60 psi (4 Bar) higher...

Gas Turbine Engineering Handbook 2 Episode 8 potx

... 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 4:02PMSteam-Cooled Turbine BladesThis ... 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 4:02PMThe value of the work factor for an impulse turbine (zero ... actual condition)3 72 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 9.3D ± 346 ± [337±369/33] 29 .10 .20 01 4:02PMFigure 9-8 shows the Ratteau turbine. The total...

Gas Turbine Engineering Handbook 2 Episode 9 potx

... required411G:/GTE/FINAL (26 -10-01)/CHAPTER 11.3D ± 421 ± [409±435 /27 ] 1.11 .20 01 3:51PMOther Oxides2Mo3O 2 3 2 MoO32W 3O 2 3 2WO34V 5O 2 3 2V 2 O5The Ni-base alloy surface is exposed to an oxidizing gas, ... 20 20 BAL 2. 5 3Â±Â±Â±Â± 0 .20 Â±Â±GTD -22 2 22 .5 BAL 19Â± 2. 0 2. 3 1 .2 0.8Â± 0.10 0.008 1.00Â±CombustorsSS309 23 13Â± BALÂ±Â±Â±Â±Â±Â± 0.10Â±Â±HAST X 22 BAL 1.5 ... 1.8Â± 2. 9Â± 0.03Â±Â±Cr-Mo-V 1 0.5Â± BALÂ± 1 .25 Â±Â±Â± 0 .25 0.30Â±Â±A286 15 25 Â± BALÂ± 1 .2 2 0.3Â± 0 .25 0.08 0.006Â±M1 52 12 2.5Â± BALÂ± 1.7Â±Â±Â± 0.3 0. 12 Â±Â±Compressor...

Gas Turbine Engineering Handbook 2 Episode 1 pptx

... overhauls.051015 20 25 303540455040.00 60.00 80.00 100.00 120 .00 140.00 160.00 180.00 20 0.00 22 0.00 24 0.00 26 0.00Net Output Work (btu/lb-air)Efficiency %1800 20 00 22 00 24 00 26 00 28 0030003000 ... 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 =5791113403015 20 17Figure 1-6. Performance map of a simple cycle gas turbine. -5.0010.0015.00 20 .00 25 .0030.0035.0040.0045.0050.00-50.00 ... turbine. -5.0010.0015.00 20 .00 25 .0030.0035.0040.0045.0050.00-50.00 100.00 150.00 20 0.00 25 0.00 300.00Net Output Work (btu/lb-air)Efficiency % 20 001800 22 00 24 00 26 00 28 0030001800 F°9 82 C° 20 00 F°1094...

Gas Turbine Engineering Handbook 2 Episode 3 pot

... obtained:V1 2  V 2 1 V 2 m1V 2 2 V 2  2  V 2 m 2 W1 2 U1À V1 2  V 2 m1W 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 h1À h 2 V1 2 2gcÀV 2 22gcZ1À Z 2 3 -24 Combining the energy and momentum equations provides the followingrelationships:h1À h 2 V1 2 2gcÀV 2 22gcZ1À ... 123 G:/GTE/FINAL (26 -10-01)/CHAPTER 3.3D ± 122 ± [1 12 140 /29 ] 1.11 .20 01 3:58PMFor isentropic flow,T2tT1tP2tP1tÀ13 -28 By combining Equations (3 -27 ) and (3 -28 ),T1t1 ÀP2tP1tÀ1451CpgcU1V1À...

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 3:57PMTable 4 -2 continued 27 . Exhaust diffuser 28 . ... costwould increase from natural gas to the heavy oils.0100 20 03004005006000 20 40 60 80 100 120 140 160 180 20 0 22 0 24 0 GAS TURBINE- FRAME TYPE-RATED POWER (MW)3031 32 3334353637EfficiencyCostEFFICIENCY ... report.148 Gas Turbine Engineering Handbook G:/GTE/FINAL (26 -10-01)/CHAPTER 3.3D ± 139 ± [1 12 140 /29 ] 1.11 .20 01 3:58PMFigure 3-19. Combined cycle and simple cycle efficiency as a function of gas turbine...

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 3:57PMis 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 27 4/56] 29 .10 .20 01 3:59PMFor nonprewhirl ... 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 5.3D ± 20 7 ± [178 21 8/41] 29 .10 .20 01...

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 3:59PMFigure 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 ± [21 9 27 4/56] 29 .10 .20 01 3:59PMScroll ... Compressors 26 1//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 6.3D ± 27 0 ± [21 9 27 4/56] 29 .10 .20 01 3:59PMFigure 6-47. Various configurations of centrifugal compressors. 27 0 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL...

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 4:00PMandW1 2  Vz1 2 Vz1tan  2  2 7-18W 2 2 Vz2 2 Vz2tan 4 2 7-19Therefore,HrVz 2 2gctan 2  2 À ... 4 2 7-19Therefore,HrVz 2 2gctan 2  2 À tan 2 4Thus, the reaction of the stage can be writtenR Vz2Utan 2  2 À tan 2 4tan  2 À tan 47 -20 Simplifying the previous equation,R Vz2Utan  2  ... (26 -10-01)/CHAPTER 8.3D ± 322 ± [319±336/18] 29 .10 .20 01 4:01PMFigure 8-3. Cantilever-type radial-inflow turbine. Figure 8-4. Mixed-flow-type radial-inflow turbine. 322 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL...

Gas Turbine Engineering Handbook 2 Episode 10 docx

... 0Â 20 .1/80Residual 0Â±1 0Â 20 0Â±100 5/400Crude 0Â±1 0Â 20 0Â± 122 .1/804 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-4Flash pointF 130/160 118Â 22 0 150 /20 0 < RT 175 /26 5 186F 198 50 /20 0Pour pointF À50 À55 to 10 À10=30 15/95 68 10F 15/110Visc. CS @ 100F 1.4 /2. 2 2. 48 /2. 67 2. 0/4.0 ... depends on many considerations,456 Gas Turbine Engineering Handbook G:/GTE/FINAL (26 -10-01)/CHAPTER 12. 3D ± 454 ± [436±466/31] 1.11 .20 01 3:52PMCleaning of Turbine ComponentsA fuel treatment...

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