MS 5001 PA Heavy Duty Gas Turbine
GE G Mark rket et Stat atus us (Dec ecem embe ber rr 200 2200 5) GE Oil Oill & Oi & Gas Gas Gas as -- Ma Mark Ma rket et St Stat St atus us (D (Dec (D ecem embe ber 2005) 005) 5)** ALGERIA ANGOLA
17 6
MEXICO NIGERIA
3 17
ARGENTINA
4
OMAN
3
BAHRAIN
1
QATAR
3
BOLIVIA
1
ROMANIA
2
CHINA
3
RUSSIAN FEDERATION
5
EQUATORIAL GUINEA
4
S. ARABIA
6
FRANCE
2
SINGAPORE
2
GUAM
2
SUDAN
2
HOLLAND
3
SWITZERLAND
1
INDIA
4
THAILAND
1
INDONESIA
5 3 20
UK IRAQ USA
1 8 24
2
U.A.E.
1
VIRGIN ISLAND
5
VIETNAM
1
IRAN ITALY KOREA LIBYA MALAYSIA
11 9
Total Units: 182 * Fleet installed from GE Energy Oil & Gas Nuovo Pignone 2/ GE / June 23, 2009
GE G Mark rket et Stat atus us (Dec ecem embe ber rr 200 2200 5) GE Oil Oill & Oi & Gas Gas Gas as -- Ma Mark Ma rket et St Stat St atus us (D (Dec (D ecem embe ber 2005) 005) 5)** ALGERIA ANGOLA
17 6
MEXICO NIGERIA
3 17
ARGENTINA
4
OMAN
3
BAHRAIN
1
QATAR
3
BOLIVIA
1
ROMANIA
2
CHINA
3
RUSSIAN FEDERATION
5
EQUATORIAL GUINEA
4
S. ARABIA
6
FRANCE
2
SINGAPORE
2
GUAM
2
SUDAN
2
HOLLAND
3
SWITZERLAND
1
INDIA
4
THAILAND
1
INDONESIA
5 3 20
UK IRAQ USA
1 8 24
2
U.A.E.
1
VIRGIN ISLAND
5
VIETNAM
1
IRAN ITALY KOREA LIBYA MALAYSIA
11 9
Total Units: 182 * Fleet installed from GE Energy Oil & Gas Nuovo Pignone 2/ GE / June 23, 2009
MS MS 5001 5001 Performance Performance history history
3/ GE / June 23, 2009
MS MS 5001 5001 Performance Performance** PG
Output (MW): Efficiency (%):
26.8
Heat rate (kj/kwh):
12,687
Pressure ratio
10.5
Firing temperature (°C):
963
Shaft speed (rpm):
5,094
Exhau Ex haust st flow flow (KG (KG/se /sec): c):
125.2
Exhaust temperature (°C):
485
28.4
ISO conditions conditions - natura naturall gas * MS 5001 PA
4/ GE / June 23, 2009
Design Design Features Features of of Accessory Accessory Equipment Equipment • High flexibility to meet specific job requirements • Single base for turbine and accessories • Wide range of configurations con figurations available with standard features that enable the systems to be adapted to suit the economic requirements of each application • Opera Operating ting flexi flexibilit bilityy – Base Base,, Mid Mid Rang Range, e, Daily Daily Start • Fuel flexibility – wide range of gas and liquid fuel (Crude Oil, LPG, Naph Naphta, ta, Refinery Refinery Fuel, Low Low Btu Fuel, etc.) etc.) • Capability of burning in a “MIX MODE” MODE” (Natural gas gas and light distillate oil) • Low capital cost • Low maintenance cost
5/ GE / June 23, 2009
Gas Gas Turbine Turbine Position Position Orientation Orientation
6/ GE / June 23, 2009
INLET CASING
7/ GE / June 23, 2009
Inlet Casing
8/ GE / June 23, 2009
Magnetic Speed Pickups Control Speed
9/ GE / June 23, 2009
Axial Compressor IGV
10 / GE / June 23, 2009
Axial Compressor IGV
Variable IGV (models N/P) Fixed IGV (old models ) 11 / GE / June 23, 2009
Axial Compressor IGV
12 / GE / June 23, 2009
Axial Compressor IGV
LVDT
MOOG
13 / GE / June 23, 2009
Water Washing Manifold
14 / GE / June 23, 2009
AXIAL COMPRESSOR
15 / GE / June 23, 2009
Axial Compressor Material:
Feature:
stages
17
Stub Shaft
NiCrMoV
stage of IGV (variable)
1
Compressor Disc
stages of EGV
2
NiCrMoV (stg. 1-15) CrMoV (stg. 16-17)
Pressure Ratio:
10,5
IGV
GTD 450
AIR FLOW (KG/sec):
123
Blade
SPEED (rpm):
5100
450 GTD (stg. 0-2) AISI 403 (stg.3-15) with coating GECC-1
stages 3 – 8
16 / GE / June 23, 2009
Axial Compressor blades
17 / GE / June 23, 2009
Axial Compressor assembly
18 / GE / June 23, 2009
Axial Compressor assembly
19 / GE / June 23, 2009
Axial Compressor Blades From 1st through 4th stage, the stator blades fit into semi-circular rings that fit into grooves in the casing wall.
20 / GE / June 23, 2009
Axial Compressor Extraction Pockets
Stage Nr 10
Stage Nr 4
21 / GE / June 23, 2009
Axial Compressor EGV
22 / GE / June 23, 2009
COMBUSTION SYSTEM
23 / GE / June 23, 2009
Combustion System description Feature:
N° chamber
10
Type
reverse flow
Burner
single, dual fuel
Firing Temperature (°C)
968
Water injection
available
Steam injection
available
DLN
available
Material:
Liner
Hastelloy X + HS188 with Thermal barrier coating
Cap
Hastelloy X + HS188
Crossfire Tube
AISI 304
Transition piece
Nimonic 263 with Thermal barrier coating
24 / GE / June 23, 2009
Typical Combustion Chambers Arrangement
Combustors may be: 1)
Standard
2)
Standard with Steam Injection*
3)
Standard with Water Injection*
4)
DLN 1 Type**
*: Wet System for NOx reduction **: Dry System for NOx reduction 25 / GE / June 23, 2009
Combustion Chambers: Cross Fire Tubes
26 / GE / June 23, 2009
Standard Combustion Chamber Assembly
27 / GE / June 23, 2009
Gas Fuel Nozzle
28 / GE / June 23, 2009
Dual Fuel Nozzle
29 / GE / June 23, 2009
Steam Inj. is available for Wet NOx Reduction
30 / GE / June 23, 2009
Flame Detector
31 / GE / June 23, 2009
Spark Plug
32 / GE / June 23, 2009
Standard Liner
33 / GE / June 23, 2009
Transition Piece
34 / GE / June 23, 2009
Transition Piece
35 / GE / June 23, 2009
TURBINE SECTION
36 / GE / June 23, 2009
Turbine Rotor Material:
Feature:
stages
2
Stub Shaft
CrMoV
Ratation
counterclockwise
Turbine Disc
M 152
Type
axial flow
Nozzle 1°stg
FSX 414
SPEED (rpm):
5100
Bucket 1°stg
GTD111
Nozzle 2°stg
N 155
Bucket 2°stg
IN 738
Vacuum plasma coating on first stage nozzle Cooling of first stage nozzles only
37 / GE / June 23, 2009
Turbine section: Parts 1st Stage Nozzle
1st Turbine wheel
2nd stage Nozzle
2nd Turbine wheel
38 / GE / June 23, 2009
Turbine Cooling
39 / GE / June 23, 2009
Turbine Cooling
40 / GE / June 23, 2009
Turbine section: 1st Stage Nozzle
41 / GE / June 23, 2009
Turbine section: 1st Stage Nozzle
42 / GE / June 23, 2009
Turbine section: 2nd Stage Nozzle
Hallow airfoilshaped partition
43 / GE / June 23, 2009
1st & 2nd Turbine wheels
This space create a seal for hot gas with turbolence
44 / GE / June 23, 2009
1st & 2nd Turbine wheels
45 / GE / June 23, 2009
1st & 2nd Turbine wheels
46 / GE / June 23, 2009
Turbine section: Shroud Block
47 / GE / June 23, 2009
EXHAUST SECTION
48 / GE / June 23, 2009
EXHAUST SECTION
49 / GE / June 23, 2009
EXHAUST SECTION
50 / GE / June 23, 2009
EXHAUST SECTION
51 / GE / June 23, 2009
EXHAUST SECTION: Turning Vanes
52 / GE / June 23, 2009
TURBINE BEARINGS
53 / GE / June 23, 2009
Gas Turbine Bearings
54 / GE / June 23, 2009
Gas Turbine Bearings
Journal
Thru st Lo ad
Thru st UnLo ad 55 / GE / June 23, 2009
Bearing Nr 1 Assembly
56 / GE / June 23, 2009
Bearing Nr 1 Assembly: THRUST BEARINGS
57 / GE / June 23, 2009
