GasTurbine Engineering HandbookSecond Edition phần 9 pot

... 3 Â ±5, 199 3. 690 Gas Turbine Engineering Handbook G:/GTE/FINAL (26-10-01)/CHAPTER 19. 3D ± 664 ± [634± 691 /58] 1.11.2001 2:38PM one considers the fact that the gas turbine ingests about 7000 Â 90 00 ... 0.704 0.218 7 0.750 0.231 8 0.788 0.240 9 0.820 0.250 10 0.848 0.260 11 0.873 0.265 12 0. 895 0.270 13 0 .90 6 0.277 14 0 .93 3 0.282 15 0 .94 8 0.287 16 0 .96 3 0. 290 Tabulation sh...

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... 0.25 86 93 % 96 98 % 12±16 Combined cycle gas turbine 600 90 0 6203±6545 55 4.0 0.35 86 93 % 95 98 % 22±24 Advanced gas turbine combined cycle power plant 800±1000 52 49 5538 65 4.5 0.4 84 90 % 94 96 % 28±30 Combined ... 0.23 88 95 % 97 99 % 10±12 Simple cycle gas turbine oil fired 400±500 8322±82 29 41 6.2 0.25 85 90 % 95 97 % 12±16 Simple cycle gas turbine crude fired 500±600 10662±11...

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... Figure 9- 18. Figure 9- 16. Film and convection-cooled blade. 356 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 9. 3D ± 346 ± [337±3 69/ 33] 29. 10.2001 4:02PM Figure 9- 8 ... approximately 20  F (10  C) per year. The 1000 1200 1400 1600 1800 2000 2200 2400 2600 2800 195 0 196 0 197 0 198 0 199 0 2000 2010 YEAR Firing Temperature F (°C)° U 500 RENE 7...

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... US$ Total Earnings US$ Evaporative cooling 3. 69 3.32 0. 39 10, 891 0.5 135.67 515,264 396 ,755 91 2,0 19 Refrigeration inlet cooling 12.77 11.51 2.5 10,672 2.5 195 .74 605,075 1,3 79, 901 1 ,98 4 ,97 7 Ice storage cooling 12.77 ... 9, 020 3.7 157.84 5, 597 ,388 3,368,355 8 ,96 5,744 Steam injection 10.11 9. 11 22.13 895 4 1.7 168. 19 5,220, 193 1,466, 792 6,686 ,98 5 Evaporative cooli...

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... year: 199 7). ASME Gas Turbine Control and Protection Systems B133.4 Published: 197 8 (Reaffirmed year: 199 7). ASME Gas Turbine Installation Sound Emissions B133.8 Published: 197 7 (Reaffirmed: 198 9). ASME ... Services, 2nd Edition, July 199 7, Reaffirmed March 2000. API Std 681, Liquid Ring Vacuum Pumps and Compressors, 1st Edition, February 199 6. ASME Basic Gas Turbines B 133.2 Publis...

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... 6-34. Recirculating loss. 254 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 6.3D ± 2 69 ± [2 19 274/56] 29. 10.2001 3:59PM weight. One must also know the corrosive ... a centrifugal compressor. 238 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 6.3D ± 2 59 ± [2 19 274/56] 29. 10.2001 3:59PM When the inlet flow to the imp...

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... A&M University; p. 1 79; 199 9. Bernstien H.L., ``Materials Issues for Users of Gas Turbines,'' Proceedings of the 27th Texas A&M Turbomachinery Symposium, ( 199 8). Lavoie, R., and ... Systems //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 10.3D ± 399 ± [370±408/ 39] 29. 10.2001 4:02PM The DLE injector has two fuel circuits. The main fuel, approximately 97 % of the total,...

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... (26-10-01)/CHAPTER 13.3D ± 492 ± [467±520/54] 1.11.2001 3:56PM Figure 13-18. Various types of thrust bearings. Figure 13- 19. Thrust-bearing temperature characteristics. 492 Gas Turbine Engineering Handbook G:/GTE/FINAL ... Technique,'' Proceedings of the 27th Turbomachinery Symposium, Texas A&M University, p. 39, 199 8. 520 Gas Turbine Engineering Handbook G:/GTE/FINAL (26...

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... 2 09, 199 1. Goodman, T.P., ``A Least-Squares Method for Computing Balance Correc- tions,'' ASME Paper No. 63-WA- 295 . Jackson, C., ``Using the Orbit to Balance,'' Mechanical Engineering, ... best to Figure 17 -9. Rotor amplitudes for least-square balance. 596 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 18.3D ± 607 ± [605±633/ 29] 2...

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... are between 94 Â 97 %, while the bigger units above 100 MW have availability factors of 85 Â ± 89% . The bigger units produce twice the output, but the avail- ability factor has decreased from 95 % to ... reli- ability is usually a greater economic factor than the high maintenance costs. 96 35 85 45 0 10 20 30 40 50 60 70 80 90 100 Below 100 MW Above 100 MW Availability Efficiency Fig...

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