GasTurbine Engineering HandbookSecond Edition phần 7 pptx
GasTurbine Engineering HandbookSecond Edition phần 7 pptx
... influences from
other components in the system.
521
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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
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Figure 13-18. Various types...
GasTurbine Engineering HandbookSecond Edition phần 3 pptx
... 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...
GasTurbine Engineering HandbookSecond Edition phần 8 pptx
... 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
"
Ft
"
Fe
i!t
17- 1
"
Yt
"
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...
GasTurbine Engineering HandbookSecond Edition phần 1 pot
... 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/...
GasTurbine Engineering HandbookSecond Edition phần 2 doc
... 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...
GasTurbine Engineering HandbookSecond Edition phần 4 doc
... 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...
GasTurbine Engineering HandbookSecond Edition phần 5 potx
... (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...
GasTurbine Engineering HandbookSecond Edition phần 6 doc
... 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...
GasTurbine Engineering HandbookSecond Edition phần 9 pot
... (%) 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
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cleaning will be...
GasTurbine Engineering HandbookSecond Edition phần 10 docx
... 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]...
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