26
 Nuovo Pignone  CLIENTE CUSTOMER Daelim FIRENZE LOCALITAPLANT LOCATION KUWAIT COMMESSA - JOB 1800057  IMPIANTO INSTALLATION KNPC 4 th 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.  St oppa L. 18/02/ 11 ITEM - 1 Revised pages 1, 8, 9, 12 R.Jagielski  Fadlun E.  St oppa L. 23/12/ 10  N. SOM54 6429 2 / 4 0 EMESSO - ISSUED R.Jagielski  Marchio ne T.  St oppa L. 29/09/ 10  LINGUA-LANG. PAGINA-SHEET REV.  DESCRIZIONE - DESCRIPTION  PREP ’D CON T. -C HK’ D AP P. -APP R ’D D AT A-DA TE  A 1 / 2 Il 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.  SOSTIT UITO 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 APPL ICABLE SIGNED 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  JAGI ELSKI R. MARCHI ONE T. STOPPA L. N/ A  18. FEB.’ 11 AD DED PAGES 10 to 23 JAG IELSKI R. M ILIANI A. STOPPA L. N/A  2 2. DE C. ’1 0 R EV I SED PAGES - 1, 8, 9, 12  JAG IELSKI R. FA DLUN E. STOPPA L. N/A  29.SEP.’10 ISSUED  JAGI ELSKI R. MARCHI ONE 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 REFINERY TITLE : G.T. PERFORMANCE CURVES REV. UNIT NO. 231 DRAWING NO. : VP-18-101-C-231-001A/B-C-001 SCALE N/A DIC PROJECT NO. 090768 ORDER 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    '

VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves

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7/18/2019 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   '

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

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

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

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

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

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

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

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

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 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

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 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

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 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

F   LINGUA-LANG. PAGINA-SHEET

REV.   DESCRIZIONE - DESCRIPTION   A 15 / 16Il 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

Max. Load; Air Flow=106%

Air Flow=82.2%; Texh=546°C

-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 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

REV.   DESCRIZIONE - DESCRIPTION   A 16 / 17Il 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

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

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 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

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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

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

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

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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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

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

REV.   DESCRIZIONE - DESCRIPTION   A 24 / 25Il 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

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

7/18/2019 VP 18 101 C 231 001AB C 001 Gas Turbines Performance Curves

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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

REV.   DESCRIZIONE - DESCRIPTION   A 25 / 26Il 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

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