VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Transcript of VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone CLIENTE – CUSTOMER
Daelim
FIRENZE LOCALITA’ – PLANT LOCATION
KUWAITCOMMESSA - JOB
1800057 IMPIANTO – INSTALLATION
KNPC 4th
LPG Train (Feed Gas Train)
TITOLO - TITLE
3 Added Approval Status Table on the 1st page R.Jagielski 14/09/11
2 Added pages – 10 to 23 R.Jagielski Miliani A. Stoppa L. 18/02/11
ITEM
-
1 Revised pages – 1, 8, 9, 12 R.Jagielski Fadlun E. Stoppa L. 23/12/10 N. SOM5464292 / 4
0 EMESSO - ISSUED R.Jagielski Marchione T. Stoppa L. 29/09/10 LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION P RE P’D CONT. -CHK ’D A PP .-AP PR’D DATA-DA TE A 1 / 2Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
Gas Turbines Performance Curves
MS5002C
Standard Combustor Combined Cycle
DAELIM INDUSTRIAL CO., LTD.
JOB NO. 090768
A1 - APPROVED
A2 - APPROVED AS NOTED
A3 - RETURN FOR CORRECTION
NA - NOT APPLICABLESIGNED BY: DATE
DAELIM PERMISSION TO PROCEED OR REVIEW TAKEN ON VENDOR PRINTS
SHALL NOT RELIEVE VENDOR FROM ITS RESPONSIBILITIES OR LIABILITIES
UNDER THE PURCHASE ORDER
14.SEP.’11 ADDED APPROVAL STATUS TABLE
on the 1st page JAGIELSKI R. MARCHIONE T. STOPPA L. N/A
18.FEB.’11 ADDED PAGES – 10 to 23 JA GIELSKI R. M ILIANI A. STOPPA L. N/A
22.DEC.’10 REVISED PAGES - 1, 8, 9, 12 JA GIELSKI R. F ADLUN E. STOPPA L. N/A
29.SEP.’10 ISSUED JAGIELSKI R. MARCHIONE T. STOPPA L. N/A
REV. DATE DESCRIPTION DRWN CHKD REVD APPRD
OWNER
ENG’G :
MFR :
PROJECT : LPG TRAIN-4 PROJECT
AT MINA AL-AHMADI REFINERYTITLE :
G.T. PERFORMANCE CURVES
REV.UNIT NO.
231DRAWING NO. :
VP-18-101-C-231-001A/B-C-001 SCALE
N/ADIC PROJECT NO.
090768ORDER NO. :
3
1
0
2
3
Marchione T. Stoppa L.
E l e c t r o n i c a
l l y a p p r o v e d d r a w .
G E
N u o v o P i g n o n e
I n t e r n a l D T - ' N '
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE -40°F (-40°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 2 / 3Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *NATURAL GAS
DESIGN OUTPUT kW 28337DESIGN HEAT RATE (LHV) kj/kW-h 12308
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09689
DESIGN AIR FLOW kg/h 443613DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -1.6 +0.610 mbar Exhaust -0.6 +0.6
V POUSA FEB.25, 1987 499HA287
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 0°F (-17.8°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 3 / 4Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *NATURAL GAS
DESIGN OUTPUT kW 28337
DESIGN HEAT RATE (LHV) kj/kW-h 12308DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09689
DESIGN AIR FLOW kg/h 443613DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -1.6 +0.610.mbar.Exhaust -0.6 +0.6
POUA FEB.26, 1987 REV.A 499HA258
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 30°F (-1.1°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 4 / 5Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *NATURAL GAS
DESIGN OUTPUT kW 28337
DESIGN HEAT RATE (LHV) kj/kW-h 12308DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09689
DESIGN AIR FLOW kg/h 443613
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -1.6 +0.610 mbar Exhaust -0.6 +0.6
V POUA FEB.26, 1987 REV.A 499HA2589
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 59°F (15°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 5 / 6Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *NATURAL GAS
DESIGN OUTPUT kW 28337
DESIGN HEAT RATE (LHV) kj/kW-h 12308DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09689
DESIGN AIR FLOW kg/h 443613DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -1.6 +0.610 mbar Exhaust -0.6 +0.6
V POUA DEC.30, 1986 499HA26
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 90°F (32.2°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 6 / 7Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *NATURAL GAS
DESIGN OUTPUT kW 28337
DESIGN HEAT RATE (LHV) kj/kW-h 12308
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09689DESIGN AIR FLOW kg/h 443613
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -1.6 +0.610 mbar Exhaust -0.6 +0.6
V POUA DEC.30, 1986 499HA261
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 120°F (48.9°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 7 / 8Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *NATURAL GAS
DESIGN OUTPUT kW 28337
DESIGN HEAT RATE (LHV) kj/kW-h 12308
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09689DESIGN AIR FLOW kg/h 443613
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -1.6 +0.610 mbar Exhaust -0.6 +0.6
V POUA FEB.26, 1987 499HA262
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 130°F (54.4°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
1 ADDITIONAL PAGE – PERFORMANCE MAP FOR POWER @ 130O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 8 / 9Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *NATURAL GAS
DESIGN OUTPUT kW 28337
DESIGN HEAT RATE (LHV) kj/kW-h 12308
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09689DESIGN AIR FLOW kg/h 443613
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -1.6 +0.610 mbar Exhaust -0.6 +0.6
20
30
40
50
60
70
80
90
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
S H A F T O U T P U T -
P E
R C E N T
427°C
482°C
543°C
560°C
VAR
IGV
VAR
COMP
SPEED
83.3%
72.4%
63.8%
560°C
54.4°C LOAD LIMIT 544°C EXH. TEMP.
L O A D T U R B I N E S P E E D - L
I M I T
PERCENT
DESIGN AIR
FLOW
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 130°F (54.4°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
1 ADDITIONAL PAGE – PERFORMANCE MAP FOR HEAT RATE @ 130O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 9 / 10Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *NATURAL GAS
DESIGN OUTPUT kW 28337
DESIGN HEAT RATE (LHV) kj/kW-h 12308
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09689DESIGN AIR FLOW kg/h 443613
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -1.6 +0.610 mbar Exhaust -0.6 +0.6
110
120
130
140
150
160
170
180
190
200
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
H E A T R A T E -
P E R C
E N T 427°C
482°C
543°C
560°C
560°C
54.4°C LOAD LIMIT 544°C EXH. TEMP.
VAR
COMP
SPEED
VAR
IGV
83.3%72.4%
63.8%
L O A D T U R B I N E S P E E D -
L I M I T
PERCENT
DESIGN
AIR FLOW
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE -40°F (-40°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR POWER @ -40O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 10 / 11Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
40
50
60
70
80
90
100
110
120
130
140
150
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
S H A F T O U T P U T -
P E R C E N T
399°C
427°C
482°C
530°C
VAR
COMP
SPEED &
IGV
PERCENT
DESIGN
AIRFLOW
L O A D T U R B I N E S P E E D -
L I M I
92.9%
121%
-40°C LOAD LIMIT 485°C EXH. TEMP.
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE -40°F (-40°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR HEAT RATE @ -40O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 11 / 12Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
90
100
110
120
130
140
150
160
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
H E A T R A T E -
P E R C
E N T
L O A D T U R B I N E S P E E D -
L I M I T
-40°C LOAD LIMIT 485°C EXH. TEMP.
Max. Load; Air Flow=121%
Air Flow=92.9%; Texh=530°C
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 0°F (-17.8°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR POWER @ 0O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 12 / 13Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
40
50
60
70
80
90
100
110
120
130
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
S H A F T O U T P U T -
P E R C E N T
399°C
427°C
482°C
540°C
VAR
COMP
SPEED &
IGV
PERCENT
DESIGN
AIRFLOW
L O A D T U R B I N E S P E E D -
L I M I
86.9%
112%
-17.8°C LOAD LIMIT 498°C EXH. TEMP.
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 0°F (-17.8°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR HEAT RATE @ 0O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 13 / 14Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
90
100
110
120
130
140
150
160
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
H E A T R A T E -
P E R C E N
T
L O A D T U R B I N E S P E E D -
L I M I T
-17.8°C LOAD LIMIT 498°C EXH. TEMP.
Air Flow=86.9%; Texh=540°C
Max. Load; Air Flow=112%
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 30°F (-1.1°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR POWER @ 30O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 14 / 15Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
30
40
50
60
70
80
90
100
110
120
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
S H A F T O U T P U T -
P E R C
E N T
399°C
427°C
482°C
546°C
VAR
COMP
SPEED &
IGV
PERCENT
DESIGN
AIRFLOW
L O A D T U R B I N E S P E E D -
L I M I
82.2%
106%
-1.1°C LOAD LIMIT 508°C EXH. TEMP.
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 30°F (-1.1°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR HEAT RATE @ 30O
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FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
90
100
110
120
130
140
150
160
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
H E A T R A T E -
P E R C E N
T
L O A D T U R B I N E S P E E D -
L I M I T
Max. Load; Air Flow=106%
Air Flow=82.2%; Texh=546°C
-1.1°C LOAD LIMIT 508°C EXH. TEMP.
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 59°F (15°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR POWER @ 59O
F LINGUA-LANG. PAGINA-SHEET
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This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
30
40
50
60
70
80
90
100
110
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
S H A F T O U T P U T -
P E R C
E N T
399°C
427°C
482°C
543°C
100%
PERCENT
DESIGN
AIRFLOW
L O A D T U R B I N E S P E E D -
L I M I
77.5%
15°C LOAD LIMIT 517°C EXH. TEMP.
VAR
COMP
SPEED &
IGV
554°C
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 59°F (15°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR HEAT RATE @ 59O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 17 / 18Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
90
100
110
120
130
140
150
160
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
H E A T R A T E -
P E R C E N
T
427°C
482°C
554°C
77.5%
L O A D T U R B I N E S P E E D -
L I M I T
PERCENT
DESIGN
AIR FLOW
100%
VAR
COMP
SPEED &
IGV
399°C
15°C LOAD LIMIT 517°C EXH. TEMP.
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 90°F (32.2°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR POWER @ 90O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 18 / 19Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
30
40
50
60
70
80
90
100
110
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
S H A F T O U T P U T -
P E R C
E N T
399°C
427°C
482°C
543°C
93.1%
PERCENT
DESIGN
AIRFLOW
L O A D T U R B I N E S P E E D -
L I M I
84.6%
32.2°C LOAD LIMIT 528°C EXH.
VAR
COMP
SPEED
560°C
72.5%
VAR
IGV
541°C
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 90°F (32.2°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR HEAT RATE @ 90O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 19 / 20Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
90
100
110
120
130
140
150
160
170
180
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
H E A T R A T E -
P E R C E N
T
427°C
482°C
560°C
VAR
COMPSPEED
VAR
IGV
84.6%72.5%
L O A D T U R B I N E S P E E D -
L I M I T
PERCENT
DESIGN
AIR FLOW
93.1%
399°C32.2°C LOAD LIMIT 528°C EXH.
541°C
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 120°F (48.9°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR POWER @ 120O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 20 / 21Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
20
30
40
50
60
70
80
90
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
S H A F T O U T P U T -
P E R C E N T
399°C
427°C
482°C
543°C
86.1%
PERCENT
DESIGN
AIRFLOW
L O A D T U R B I N E S P E E D -
L I M I
77.5%
48.9°C LOAD LIMIT 538°C EXH.
VAR
COMP
SPEED
560°C
67.4%
VAR
IGV
552°C
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 120°F (48.9°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR HEAT RATE @ 120O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 21 / 22Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
This document is the property of NUOVO PIGNONE . All rights are reserved according to law. SOSTITUITO DA REPLACED BY
FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
100
110
120
130
140
150
160
170
180
190
200
210
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
H E A T R A T E -
P E R C E N
T 427°C
482°C
560°C
VAR
COMP
SPEED
VAR
IGV 77.5%
67.4%
L O A D T U R B I N E S P E E D -
L I M I T
PERCENT
DESIGN
AIR FLOW
86.1%
399°C
48.9°C LOAD LIMIT 538°C EXH.
552°C
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 130°F (54.4°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR POWER @ 130O
F LINGUA-LANG. PAGINA-SHEET
REV. DESCRIZIONE - DESCRIPTION A 22 / 23Il presente documento è di proprietà NUOVO PIGNONE . A termine di legge ogni diritto è riservato. SOSTITUISCE IL – REPLACES
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FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
10
20
30
40
50
60
70
80
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
S H A F T O U T P U T -
P E R C
E N T
399°C
427°C
482°C
543°C
83.5%
PERCENT
DESIGN
AIRFLOW
L O A D T U R B I N E S P E E D -
L I M I
75.1%
54.4°C LOAD LIMIT 541°C EXH.
VAR
COMP
SPEED
560°C
65.6%
VAR
IGV
556°C
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
ESTIMATED PERFORMANCE
COMPRESSOR INLET TEMPERATURE 130°F (54.4°C)
COMPRESSOR INLET PRESSURE 14.7 PSIA (1.0133 bar)
ITEM
N. SOM5464292 / 4
2 ADDITIONAL PAGE – PERFORMANCE MAP FOR HEAT RATE @ 130O
F LINGUA-LANG. PAGINA-SHEET
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FUEL *DISTILLATE#2
DESIGN OUTPUT kW 26727
DESIGN HEAT RATE (LHV) kj/kW-h 13030
DESIGN HEAT CONSUMPTION (LHV) 10-6 kW 0.09698DESIGN AIR FLOW kg/h 442045
DESIGN SHAFT SPEED RPM 4670
Notes:1. Altitude correction on curve
418HA418.2. Ambient temperature correction
on curve 499HA2403. Pressure drop effects:
4. For additional 4” H2O pressuredrop increase exhaust temp.by 1,11 °C
5. Operation on max exhausttemp. control
% Effects PPB062786kW HR
10 mbar Inlet -2.1 +0.910 mbar Exhaust -1.1 +0.9
105
115
125
135
145
155
165
175
185
195
205
215
40 50 60 70 80 90 100 110
LOAD TURBINE SHAFT SPEED - PERCENT
H E A T R A T E -
P E R C E N T
427°C
482°C
560°C
VAR
COMP
SPEED
VAR
IGV
75.1%
65.6%
L O A D T U R B I N E S P E E D -
L I M I T
PERCENT
DESIGN
AIR FLOW
83.5%
399°C
54.4°C LOAD LIMIT 541°C EXH.
556°C
7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves
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Nuovo Pignone FIRENZE
GENERAL ELECTRIC MODEL M5382C GAS TURBINEEFFECT OF COMPRESSOR INLET TEMPERATURE ONMAXIMUM OUTPUT, HEAT RATE AND AIR FLOW
ITEM
N. SOM5464292 / 4
LINGUA-LANG. PAGINA-SHEET
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NOTES: COMPRESSOR SPEED 5100 RPM (100%)LOAD TURBINE SPEED 4670 RPM (100%)
COMBINED CYCLE
70
80
90
100
110
120
130
140
-7 4 16 27-29-40
482
493
504
516
527
538
549
POWER OUTPUT
HEAT CONSUMP.AIRFLOW
HEAT RATE
BASE LOAD EXHAUST TEMPERATURE CURVE
COMPRESSOR INLET TEMPERATURE (°C)
P E R C E N T D E S I G N
E X H A U S T T E M
P E R A T U R E ( ° C )
-18 38 49 54
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Nuovo Pignone FIRENZE
GAS TURBINE ALTITUDE CORRECTION FACTOR FOR
OUTPUT AND HEAT CONSUMPTION AND
ALTITUDE VS. ATMOSPHERIC PRESSURE
ITEM
N. SOM5464292 / 4
LINGUA-LANG. PAGINA-SHEET
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NOTES: 1. ALTITUDE PRESSURE CALCULATED BY METHODS OF NACA REPORT NO. 218.2. HEAT RATE AND THERMAL EFFICIENCY UNAFFECTED BY ALTITUDE.
0
0.70
0.80
0.90
1.00
A L T I T U D E
C O R R E C
T I O N F A C T O
R
A L T I T U D E C O R R E C T I O N F A C T O R
A
L T I T U D E ( m )
1.014 0.965 0.896 0.827 0.758
610
914
1219
1524
1829
2134
2438
ATMOSPHERIC PRESSURE - bar absGAS TURBINE DEPT.
305
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Nuovo Pignone FIRENZE
GAS TURBINE CORRECTION FACTOR FOR SHAFT OUTPUT AND
HEAT RATE VALUES DUE TO SPECIFIC HUMIDITY
ITEM
N. SOM5464292 / 4
ADDITIONAL PAGE HUMIDITY CORRECTION FACTOR LINGUA LANG PAGINA SHEET
Correction To Output and Heat Rate
For Non Iso Specific Humidity Conditions
0.994
0.995
0.996
0.997
0.998
0.999
1.000
1.001
1.002
1.003
1.004
1.005
1.006
1.007
1.008
1.009
1.010
0.000 0.005 0.010 0.015 0.020 0.025 0.030 0.035
Specific Humidity [lb. water vapor/lb. Dry air]
C o r r e c t i o n F a c t o r
Heat Rate
Power Output
ISO Specific Humidity
0.0064 lb.water/lb.dry air