Gas Turbine Engineering Handbook 2 Episode 9 potx

... 7Â±Â±Â±Â±Â± 0 .25 0.01Â±N155 21 20 20 BAL 2. 5 3Â±Â±Â±Â± 0 .20 Â±Â±GTD -22 2 22 .5 BAL 19 Â± 2. 0 2. 3 1 .2 0.8Â± 0.10 0.008 1.00Â±CombustorsSS3 09 23 13Â± BALÂ±Â±Â±Â±Â±Â± ... required411G:/GTE/FINAL (26 -10-01)/CHAPTER 11.3D ± 421 ± [4 09 435 /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, ... 0.10Â±Â±HAST X 22 BAL 1.5 1 .9 0.7 9 Â±Â±Â±Â± 0.07 0.005Â±N -26 3 20 BAL 20 0.4Â± 6 2. 1 0.4Â±Â± 0.06Â±Â±HA-188 22 22 BAL 1.5 14.0Â±Â±Â±Â±Â± 0.05 0.01Â± Turbine WheelsAlloy...

Gas Turbine Engineering Handbook 2 Episode 8 potx

... (4 72 C), approximately 20 F (10C) per year. The1000 120 0140016001800 20 00 22 00 24 00 26 00 28 00 195 0 196 0 197 0 198 0 199 0 20 00 20 10YEARFiring Temperature F (°C)°U 500RENE 77IN 733GTD111GTD ... NASA, TM X -21 76, 197 1.Figure 9 - 29 . Turbine performance map.Axial-Flow Turbines 367//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 9. 3D ± 355 ± [337±3 69/ 33] 29 .10 .20 01 4:02PMFigure 9- 14. Strut ... loss.366 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 9. 3D ± 3 62 ± [337±3 69/ 33] 29 .10 .20 01 4:02PMCooled -Turbine AerodynamicsThe injection of coolant air in the turbine...

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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°1 094 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°16 49 C°Pr = 57 9 111315 20 304017Figure 2- 17. ... sacrificing alloy corrosion resistance; and advanced, highly1000 120 0140016001800 20 00 22 00 24 00 26 00 28 00 195 0 196 0 197 0 198 0 199 0 20 00 20 10YEARFiring Temperature ºF (ºC)U 500RENE 77 IN 733 GTD111GTD ... 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°1 094 ...

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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°16 49 ... F°16 49 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°1 094 C°1800 F° 9 82 C°Pr =57 9 1113403015 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°1 094 ...

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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 ... US$TotalEarningsUS$Evaporativecooling3. 69 3. 32 0. 39 10, 891 0.5 135.67 515 ,26 4 396 ,755 9 12, 0 19 Refrigerationinlet cooling 12. 77 11.51 2. 5 10,6 72 2.5 195 .74 605,075 1,3 79, 901 1 ,98 4 ,97 7Ice storagecooling 12. 77 11.51 2. 5 10,6 72 1.5 ... 117.44 20 1,6 92 4 59, 967 661,6 59 Inter-stagecompressorcooling17.41 15. 69 14. 19 9,576 2. 5 143.56 3,743,308 2, 291 ,365 6,034,6 72 Heated andhumidifiedcompressedair injection 23 .44 21 . 12 21 .23 9, 020 ...

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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 . ... report.148 Gas Turbine Engineering Handbook G:/GTE/FINAL (26 -10-01)/CHAPTER 3.3D ± 1 39 ± [1 12 140 / 29 ] 1.11 .20 01 3:58PMFigure 3- 19. Combined cycle and simple cycle efficiency as a function of gas turbine ... 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...

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Gas Turbine Engineering Handbook 2 Episode 5 pps

... 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 ... 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 ... Journal of Engineering for Power, ASMETrans., Vol. 86, Series A, p. 22 7.)Centrifugal Compressors 22 3//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 6.3D ± 23 2 ± [21 9 27 4/56] 29 .10 .20 01 3:59PM3....

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Gas Turbine Engineering Handbook 2 Episode 6 pps

... Diesel and Gas Turbine Worldwide, October 198 8, pp. 46Â±50. 27 2 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 6.3D ± 23 9 ± [21 9 27 4/56] 29 .10 .20 01 3:59PMCoriolis ... 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 profiles ... lift and drag forces on an airfoil. 28 2 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 6.3D ± 25 9 ± [21 9 27 4/56] 29 .10 .20 01 3:59PMWhen the inlet flow to the impeller...

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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 ... (26 -10-01)/CHAPTER 8.3D ± 322 ± [3 19 336/18] 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 ... Blade Row,'' NACA RM E54 120 ( 195 4).318 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 7.3D ± 29 1 ± [27 5±318/44] 29 .10 .20 01 4:00PM40:1. Figure 7-3 shows...

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Gas Turbine Engineering Handbook 2 Episode 10 docx

... .7543@60F . 92 / 1.05 .84 .874 .8786 .80/. 92 Water & ded. 0 .1%wtHeating valueBtulb 19, 300/ 19, 70018,330 19, 000/ 19, 600 18,700/18, 820 18,300/18 ,90 0 18 ,25 0 18 ,23 9 19, 000/ 19, 400Hydrogen % 12. 8/14.5 ... #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 ... 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...

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