DWG Number 111T3762 Rev - Released 2/21/2014 Page 1 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Gas Turbine Generator(s) ONLY

Reference Conditions and Corresponding Correction Curves

Units
Fuel Gas Design data at reference conditions
Fuel LHV kJ/kg See gas constituents Units Values
Load Base & Part Gen Term Output kW 130311
Diluent Injection Fluid None Heat Rate LHV kJ/kWh 10437
Generator Frequency Hz 50 Exhaust Temp °C 546.7
Generator Power Factor ratio 0.80 Exhaust Flow t/h 1495.6
Cycle Deck Version Used PG9171-05A-1111

Applicable Correction Curve Sheet Numbers

Summary Page Sheet 1

Reference Exhaust DP Sheet 2

Units Value Output Heat Rate Exhaust Flow Exhaust Temperature Heat Consumption
Ambient Temperature °C 15 Sheet 3 Sheet 4 Sheet 5 Sheet 6 Sheet 7
Ambient Relative Humidity % 60 Sheet 8 Sheet 9 Sheet 10 Sheet 11 Sheet 12
Barometric Pressure mbara 1013.5 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17
Shaft Speed rpm 3000 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22
Fuel Temperature °C 27 Sheet 23 Sheet 24 N/A N/A Sheet 25
Inlet Diff Pressure (On CC or @Tf) mmH2O 89 Sheet 26 Sheet 27 Sheet 28 Sheet 29 Sheet 30
Exhaust Pressure (On Control Curve) mmH2O 127 Sheet 31 Sheet 32 N/A Sheet 33 Sheet 34
Fuel gas composition See gas constituents Sheet 35 Sheet 36 Sheet 37 Sheet 38 Sheet 39
Percent Load % N/A Sheet 40 Sheet 41 Sheet 42 Sheet 43

Fuel composition (Used for Gas Fuel) Units Value Additional Notes:
Methane (CH4) % mol 100.00 % Inlet Bleed Heat included and operating on a normal control schedule
Gas Fuel LHV - per ASTM D3588 kJ/kg 50035
Gas Fuel H/C Ratio ratio 4.00 Pre-Integrated Tuning Correction Curves
LHV is given for information only, gas composition is the reference. FOR INFORMATION ONLY - NOT GUARANTEED

NOTE: These performance curves are provided for reference only and do not constitute performance guarantees at any conditions other than those listed in
the contract. An additional set of site-specific curves will be issued before the performance test to which the measured performance from test conditions will
be corrected.
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 COT Application: Version 1.35 Sheet 1

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 2 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Ambient Temperature on Exhaust Pressure
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY

 









      












This curve is used as reference curve for
exhaust backpressure correction.










      
      

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 2
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 3 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Ambient Temperature on Output
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY
















 









 
Curve generated with design compressor
  inlet relative humidity.

 

 







      
      

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 3
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 4 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Ambient Temperature on Heat Rate
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY












   








Curve generated with design compressor
inlet relative humidity.








      
      

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 4
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 5 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Ambient Temperature on Exhaust Flow
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY














  









 Curve generated with design compressor

inlet relative humidity.


 



      
      

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 5
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 6 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Ambient Temperature on Exhaust Temperature
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY








   
  ! 




Curve generated with design compressor
inlet relative humidity.









      
      

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 6
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 7 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Ambient Temperature on Heat Consumption
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY












   










Curve generated with design compressor
inlet relative humidity.


 

 

 



      
      

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 7
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 8 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Relative Humidity on Output at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY














 



















 
          
 " #$  %
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 8
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 9 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Relative Humidity on Heat Rate at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY











 







   















 

 

 
          
 " #$  %
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 9
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 10 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Relative Humidity on Exhaust Flow at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY










  














 



 
          
 " #$  %
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 10
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 11 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Relative Humidity on Exhaust Temperature at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY



 









 
   
  ! 
























          
 " #$  %
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 11
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 12 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Relative Humidity on Heat Consumption at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY
















   












          
 " #$  %
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 12
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 13 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Barometric Pressure on Output at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY
















 












           
& !    
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 13
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 14 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Barometric Pressure on Heat Rate at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY














   


















 

 


 
           
& !    
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 14
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 15 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Barometric Pressure on Exhaust Flow at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY
















  












           
& !    
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 15
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 16 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Barometric Pressure on Exhaust Temperature at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY








   
  ! 























           
& !    
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 16
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 17 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Barometric Pressure on Heat Consumption at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY








 





   












           
& !    
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 17
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 18 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Shaft Speed on Output at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY






 

 





 














          
' ' #  
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 18
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 19 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Shaft Speed on Heat Rate at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY

















   












 






          
' ' #  
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 19
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 20 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Shaft Speed on Exhaust Flow at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY





 

 







  










 

 





 

 
          
' ' #  
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 20
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 21 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Shaft Speed on Exhaust Temperature at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY


   
  ! 















          
' ' #  
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 21
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 22 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Shaft Speed on Heat Consumption at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY

















   








 

 





 

 
          
' ' #  
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 22
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 23 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Fuel Temperature on Output
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY












 












        
      

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 23
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 24 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Fuel Temperature on Heat Rate
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY










   












        
      

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 24
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 25 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Fuel Temperature on Heat Consumption
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY










   














        
      

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 25
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 26 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Inlet Differential Pressure on Output at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY












 














Effects shown are for operation on the control curve. 




           
( 
      
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 26
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 27 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Inlet Differential Pressure on Heat Rate at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY



















   







 

 



 Effects shown are for operation on the control curve.

 

 
           
( 
      
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 27
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 28 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Inlet Differential Pressure on Exhaust Flow at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY










  










Effects shown are for operation on the control curve.




 
           
( 
      
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 28
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 29 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Inlet Differential Pressure on Exhaust Temperature at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY




 







   
  ! 















Effects shown are for operation on the control curve.




           
( 
      
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 29
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 30 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Inlet Differential Pressure on Heat Consumption at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY












   














Effects shown are for operation on the control curve.








           
( 
      
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 30
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 31 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Exhaust Pressure on Output at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY












 












Delta Exhaust DP = Measured Exh DP - Reference Exh DP
where: Reference Exh DP is determined per Sheet 2 
Effects shown are for operation on the control curve.
 










      

 
      
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 31
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 32 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Exhaust Pressure on Heat Rate at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY



 














   







 

 


Delta Exhaust DP = Measured Exh DP - Reference Exh DP
 where: Reference Exh DP is determined per Sheet 2
Effects shown are for operation on the control curve.
 

 





      

 
      
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 32
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 33 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Exhaust Pressure on Exhaust Temperature at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY










   
  ! 








Delta Exhaust DP = Measured Exh DP - Reference Exh DP
where: Reference Exh DP is determined per Sheet 2
Effects shown are for operation on the control curve.







      

 
      
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 33
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 34 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Exhaust Pressure on Heat Consumption at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY












   













Delta Exhaust DP = Measured Exh DP - Reference Exh DP

 where: Reference Exh DP is determined per Sheet 2
Effects shown are for operation on the control curve.

 

 

 





      

 
      
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 34
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 35 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Fuel Gas Composition on Output at Different H/C Ratios
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY

 











 




 










 
                      
  )   *+,*-

NOTES: H/C ratio is the atom ratio of the combustible components of the gas fuel. Heating Value
calculated per ASTM D3588. (1013.253 mbars, 15.56 °C)

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 35
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 36 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Fuel Gas Composition on Heat Rate at Different H/C Ratios
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY








 
   














                      
  )   *+,*-

NOTES: H/C ratio is the atom ratio of the combustible components of the gas fuel. Heating Value
calculated per ASTM D3588. (1013.253 mbars, 15.56 °C)

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 36
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 37 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Fuel Gas Composition on Exhaust Flow at Different H/C Ratios
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY



 









  












                      
  )   *+,*-

NOTES: H/C ratio is the atom ratio of the combustible components of the gas fuel. Heating Value
calculated per ASTM D3588. (1013.253 mbars, 15.56 °C)

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 37
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 38 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Fuel Gas Composition on Exhaust Temperature at Different H/C Ratios
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY








   
  ! 




 











                      
  )   *+,*-

NOTES: H/C ratio is the atom ratio of the combustible components of the gas fuel. Heating Value
calculated per ASTM D3588. (1013.253 mbars, 15.56 °C)

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 38
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 39 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Fuel Gas Composition on Heat Consumption at Different H/C Ratios
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Base
Gas Turbine Generator(s) ONLY














   








 













                      
  )   *+,*-

NOTES: H/C ratio is the atom ratio of the combustible components of the gas fuel. Heating Value
calculated per ASTM D3588. (1013.253 mbars, 15.56 °C)

Created by: Verified by: Approved by:

Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 39
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 40 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Partial Load on Heat Rate at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Part
Gas Turbine Generator(s) ONLY








   














 



           
 !  .#  ' #  %
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 40
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 41 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Partial Load on Exhaust Flow at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Part
Gas Turbine Generator(s) ONLY


















  


 

 





 

 




           
 !  .#  ' #  %
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 41
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 42 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Partial Load on Exhaust Temperature at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Part
Gas Turbine Generator(s) ONLY



 

 
 








    



 

 







 

 
           
 !  .#  ' #  %
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 42
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR

DWG Number 111T3762 Rev - Released 2/21/2014 Page 43 of 43

General Electric Model 9E Gas Turbine

9E Advanced Gas Path (AGP) Standard Curves : DLN - Natural Gas
Estimated Performances
Effect of Partial Load on Heat Consumption at Different Ambient Temperatures
Design Values Referenced on 111T3762 - - - Sheet 1
Fuel: Gas
Mode: Part
Gas Turbine Generator(s) ONLY














   









           
 !  .#  ' #  %
Created by: Verified by: Approved by:
Starzyk, Gaétan Cousin, Rémi Sesmat, Alexis 111T3762 - -
05 Feb. 2014 Sheet 43
This document contains GE proprietary information and may not be used or disclosed to others except with written permission of the GE company.

GE Proprietary Information - Class II (Internal) US EAR - NLR