GasTurbine Engineering HandbookSecond Edition phần 7 pptx

... influences from other components in the system. 521 G:/GTE/FINAL (26-10-01)/CHAPTER 13.3D ± 477 ± [4 67 520/54] 1.11.2001 3:56PM This groove or channel covers an arc of 135  and terminates abruptly in ... rotation. Figure 13-6. Comparison of general bearing types. Bearings and Seals 477 G:/GTE/FINAL (26-10-01)/CHAPTER 13.3D ± 492 ± [4 67 520/54] 1.11.2001 3:56PM Figure 13-18. Various types...

Ngày tải lên: 08/08/2014, 17:20

... continued on next page 172 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 4.3D ± 173 ± [141± 177 / 37] 29.10.2001 3:57PM Table 4-2 continued 27. Exhaust diffuser 28. ... (26-10-01)/CHAPTER 4.3D ± 177 ± [141± 177 / 37] 29.10.2001 3:57PM API Std 619, Rotary-Type Positive Displacement Compressors for Petroleum, Chemical, and Gas Industry Services, 3rd Editio...

Ngày tải lên: 08/08/2014, 17:20

... details of critical frequencies. 578 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 17. 3D ± 589 ± [584±604/21] 29.10.2001 4:06PM Figure 17- 4. Evacuation chamber for ... is " Ft " Fe i!t  17- 1 " Yt " Ae i!tÀ  17- 2 " A  " F=K 1 À ! ! n  2 i2 ! ! n   17- 3   tan À1 2 ! ! n  1 À ! ! n  2  17- 4 wh...

Ngày tải lên: 08/08/2014, 17:20

... 28±30 Combined cycle coal gasification 1200±1400 6950 73 32 49 7. 0 1.45 75 ±85% 90±95% 30±36 Combined cycle fluidized bed 1200±1400 73 00 77 01 47 7.0 1.45 75 ±85% 90±95% 30±36 Nuclear power 1800±200 10000±10550 ... engine generator power plant 650 75 0 73 00 77 01 47 5.2 4 .7 92±96% 96±98% 12±16 8 Gas Turbine Engineering Handbook G:/GTE/FINAL (26-10-01)/CHAPTER 1.3D ± 36 ± [1± 57/...

Ngày tải lên: 08/08/2014, 17:20

... 135. 67 515,264 396 ,75 5 912,019 Refrigeration inlet cooling 12 .77 11.51 2.5 10, 672 2.5 195 .74 605, 075 1, 379 ,901 1,984, 977 Ice storage cooling 12 .77 11.51 2.5 10, 672 1.5 1 17. 44 201,692 459,9 67 661,659 Inter-stage compressor cooling 17. 41 ... 661,659 Inter-stage compressor cooling 17. 41 15.69 14.19 9, 576 2.5 143.56 3 ,74 3,308 2,291,365 6,034, 672 Heated and humidified co...

Ngày tải lên: 08/08/2014, 17:20

... split Single stage (single-suction) Overhung 30 (2. 07) 250,000 (7, 079 ) 10,000 (7, 4 57) Pipeline 1200 (82) 25,000 (70 8) 20,000 (14,914) Multistage More than 5500 ( 379 ) 20,000 (566) 15,000 (11,185) Figure 6-45. ... because Centrifugal Compressors 269 //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 7. 3D ± 277 ± [ 275 ±318/44] 29.10.2001 4:00PM Figure 7- 2. Coordinate system for axial-f...

Ngày tải lên: 08/08/2014, 17:20

... (26-10-01)/CHAPTER 7. 3D ± 316 ± [ 275 ±318/44] 29.10.2001 4:00PM Figure 7- 37. High-pressure bleed chamberÐ8000 rpm. Figure 7- 38. High-pressure bleed chamberÐ9400 rpm. Figure 7- 39. Fifth-stage bleed ... Velocity o Figure 9 -7. Pressure and velocity distributions in a Curtis-type impulse turbine. 346 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 7. 3...

Ngày tải lên: 08/08/2014, 17:20

... 18.5 Â ± Â ±433 Â ± Â ± 0. 07 0.006 Â ± RENE 77 (U700) 15 BAL 17 Â ± Â ± 5.3 3.35 4.25 Â ± Â ± 0. 07 0.02 Â ± IN738 16 BAL 8.3 0.2 2.6 1 .75 3.4 3.4 0.9 Â ± 0.10 0.001 1 .75 GTD111 14 BAL 9.5 Â ± 3.8 1.5 4.9 ... Na 2 SO 4 NaÐfrom NaCl (salt) SÐfrom fuel 420 Gas Turbine Engineering Handbook //INTEGRA/B&H/GTE/FINAL (26-10-01)/CHAPTER 10.3D ± 4 07 ± [ 370 ±408/39] 29.10.2001 4:02PM T...

Ngày tải lên: 08/08/2014, 17:20

... (%) T 2 Sensitivity (%) 6 0 .70 4 0.218 7 0 .75 0 0.231 8 0 .78 8 0.240 9 0.820 0.250 10 0.848 0.260 11 0. 873 0.265 12 0.895 0. 270 13 0.906 0. 277 14 0.933 0.282 15 0.948 0.2 87 16 0.963 0.290 Tabulation ... program Figure 19-22. Savings versus efficiency. 686 Gas Turbine Engineering Handbook G:/GTE/FINAL (26-10-01)/CHAPTER 19.3D ± 677 ± [634±691/58] 1.11.2001 2:38PM cleaning will be...

Ngày tải lên: 08/08/2014, 17:20

... deter- mined at 1350  F ( 375  C) with service time for forged Inconel X -75 0 blades. Maintenance Techniques 76 1 G:/GTE/FINAL (26-10-01)/CHAPTER 21.3D ± 75 7 ± [72 2 77 7/56] 1.11.2001 4:00PM Thrust-Bearing ... finally occurs, it creates an Figure 21- 17. Damaged crossover tubes. FPO 77 0 Gas Turbine Engineering Handbook G:/GTE/FINAL (26-10-01)/CHAPTER 21.3D ± 74 2 ± [72 2 77 7/56]...

Ngày tải lên: 08/08/2014, 17:20