Gas Turbine Engineering Handbook 2 Episode 12 ppt
Gas Turbine Engineering Handbook 2 Episode 1 pptx
... F:/GTE/FINAL (26 -10 - 01) /FRONT MATTER.3D ± 1 ± [1 16 /16 ] 1. 11 .20 01 12 : 46PM
Ga sTurbine
Engineering
Ha ndbook
Second Edition
G:/GTE/FINAL (26 -10 - 01) /CHAPTER 1. 3D ± 16 ± [1 57/57] 1. 11 .20 01 3:42PM
Categories ... http://www.gulfpp.com
10 987654 3 21
Printed in the United States of America
F:/GTE/FINAL (26 -10 - 01) /FRONT MATTER.3D ± 2 ± [1 16 /16 ] 1. 11 .2...
Gas Turbine Engineering Handbook 2 Episode 2 potx
... (btu/lb-air)
Efficiency %
20 00
1800
22 00
24 00
26 00
28 00
3000
1800 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 = 5
7
9
11
13
15
20
30
40
17
Figure 2- 17. ... following:
h
4
m
a
m
f
h
4a
m
s
h
4s
=
m
a
m
f
m
s
2- 30
0
5
10
15
20
25
30
35
40
45
50
50.00 100.00 150.00 20...
Gas Turbine Engineering Handbook 2 Episode 3 pot
... Figure 3- 3, the following relationships
are obtained:
V
1
2
V
2
1
V
2
m
1
V
2
2
V
2
2
V
2
m
2
W
1
2
U
1
À V
1
2
V
2
m
1
W
2
2
U
2
À V
2
2
V
2
m
2
3 -21
Figure 3- 3. Velocity ... 117.44 20 1,6 92 459,967 661,659
Inter-stage
compressor
cooling
17.41 15.69 14.19 9,576 2. 5 1 43. 56 3, 7 43, 308 2, 291 ,36 5 6, 034 ,6 72
He...
Gas Turbine Engineering Handbook 2 Episode 4 pot
... above
Figure 4- 7. Fuel systems 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 3:57PM
Table 4 -2 continued
27 . ... lowest. Table 4- 1 shows how the maintenance cost
would increase from natural gas to the heavy oils.
0
100
20 0
300
40 0
500
600
0 20 40 60 80 100 120 140...
Gas Turbine Engineering Handbook 2 Episode 5 pps
... Compressors 23 1
//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 5. 3D ± 21 6 ± [178 21 8/41] 29 .10 .20 01 3 :57 PM
Figure 5 -28 . Campbell diagram of tested impeller.
21 6 Gas Turbine Engineering Handbook
... 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 :57 PM
i...
Gas Turbine Engineering Handbook 2 Episode 6 pps
... 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 3:59PM
Figure 6- 18. Velocity profiles ... changes.
Figure 6 -29 . Jet-wake flow distribution from an impeller.
24 6 Gas Turbine Engineering Handbook
//INTEGRA/B&H/GTE/FINAL ( 26 -10-01)/CHAP...
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 4:00PM
and
W
1
2
V
z1
2
V
z1
tan
2
2
7- 18
W
2
2
V
z2
2
V
z2
tan
4
2
7- 19
Therefore,
H
r
V
z
2
2g
c
tan
2
2
À ... diagram.
29 8 Gas Turbine Engineering Handbook
//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 7. 3D ± 3 02 ± [...
Gas Turbine Engineering Handbook 2 Episode 8 potx
... (4 72
C), approximately 20
F (10
C) per year. The
1000
120 0
1400
1600
180 0
20 00
22 00
24 00
26 00
28 00
1950 1960 1970 1 980 1990 20 00 20 10
YEAR
Firing Temperature F (°C)°
U 500
RENE 77
IN 733
GTD111
GTD ... Blades,'' NASA, TM X -21 33, 1970.
3 68 Gas Turbine Engineering Handbook
//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 9.3D ± 361 ± [337±369/3...
Gas Turbine Engineering Handbook 2 Episode 9 potx
... 7
Â
±
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±
Â
±
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±
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± 0 .25 0.01
Â
±
N155 21 20 20 BAL 2. 5 3
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±
Â
±
Â
±
Â
± 0 .20
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±
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±
GTD -22 2 22 .5 BAL 19
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± 2. 0 2. 3 1 .2 0.8
Â
± 0.10 0.008 1.00
Â
±
Combustors
SS3 09 23 13
Â
± BAL
Â
±
Â
±
Â
±
Â
±
Â
±
Â
± ... G:/GTE/FINAL (26 -10-01)/CHAPTER 11.3D ± 421 ± [4 09 435 /27 ] 1.11 .20 01 3:51PM
Other Oxides
2Mo3O
2
3 2 MoO
3
2W 3O
2
3 2WO
3
4V 5O
2
3 2V
2
O
5...
Gas Turbine Engineering Handbook 2 Episode 10 docx
... 12. 8/14.5 12. 83 12/ 13 .2 14.75 10/ 12. 5 12. 40 12/ 13 .2
Carbon residue
10% bottoms
.01/.1 .104 .03/.3 2/ 10 .3/3
Ash ppm 1/5 .001 0 /20 100 /1,000 36ppm 20 /20 0
Na K ppm 01.5 0/1 1/350 2. 2/4.5 0/50
V ... #2 Oil #2 JP-4
Flash point
F 130/160 118
Â
22 0 150 /20 0 < RT 175 /26 5 186
F 198 50 /20 0
Pour point
F À50 À55 to 10 10= 30 15/95 68 10
F 15/ 110
Visc....
Gas Turbine Engineering Handbook 2 Episode 11 doc
... (381mm)
BEARING
12 INCH (305mm)
BEARING
SHAFT SPEED RPM ì 10
–3
024 6810
12
0
100
(75)
20 0
(149)
300
(22 4)
400
(29 9)
Figure 13 -20 . Total power loss in thrust bearings.
494 Gas Turbine Engineering Handbook
... educted gas in the process.
Figure 13- 32. Multiple combination segmented gas seal system.
5 12 Gas Turbine Engineering Handbook
//INTEGRA/B&H/GTE/F...
Gas Turbine Engineering Handbook 2 Episode 12 ppt
... signature to
signature before overhaul.
5 82 Gas Turbine Engineering Handbook
//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 16.3D ± 567 ± [558±583 /26 ] 29 .10 .20 01 4:05PM
The second limitation of this ... high-pressure
air into the spray nozzle manifold.
536 Gas Turbine Engineering Handbook
//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 16.3D ± 568 ± [558±583 /26 ] 29...
Gas Turbine Engineering Handbook 2 Episode 13 ppt
... heat
Figure 18 -2. Gear coupling (male teeth integral with the hub).
608 Gas Turbine Engineering Handbook
//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 18.3D ± 613 ± [605±633 /29 ] 29 .10 .20 01 4:06PM
Sludge ... the phase angle in an elliptic orbit.
5 92 Gas Turbine Engineering Handbook
//INTEGRA/B&H/GTE/FINAL (26 -10-01)/CHAPTER 18.3D ± 621 ± [605±633 /29 ] 29 .10...
Gas Turbine Engineering Handbook 2 Episode 14 pot
... continuously.
0
20
40
60
80
100
120
0
2
4
6
8
10
12
14
Time in Minutes
Percent of Parameters (%)
Flow
Power
Firing Temperature
Speed
Figure 19-6. A typical shutdown curve for a gas turbine.
6 42 Gas Turbine Engineering Handbook
... with many composite
646 Gas Turbine Engineering Handbook
G:/GTE/FINAL (26 -10-01)/CHAPTER 19.3D ± 6 42 ± [634±691/58] 1.11 .20 01...
Gas Turbine Engineering Handbook 2 Episode 17 ppt
... 301
Â
±3
Inducers, 23 6
Â
±7
camberlines, 23 6, 27 8
Â
±9
inlet (impeller eye), 23 0
systems, 22 5
Inlet guide vanes, 22 9
Â
± 32
nonprewhirl, 23 0
prewhirl, 22 9
Â
± 32
types, 22 9
Â
± 32
Influence coefficient method, ... 427
forgings and nondestructive
testing, 427
Â
±9
gas turbine, 422
Â
±7
turbine wheel alloys, 425
Â
±7
gas turbine materials, 422
Â
±7
general met...