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 Technical Specification for     
PG6581B Gas Turbine Generating Set 
 1.         
 Manufacturing        
The gas turbine generating set is produced under Manufacture         
Associate Agreement with GE Company of     
 2.  
Structure        
PG6581B gas turbine generating set is a package unit and can be         
installed for outdoor operation. It is composed of four blocks i.e. the     
gas turbine and accessories compartment, control compartment, load gear box     
enclosure and generator compartment.        
The control panel of gas turbine, control panel and protection panels of     
generator, motor control center ( M.C.C. ) are located in the control         
compartment. Neutral point and outgoing leads cabinet are situated at     
each sides of the generator compartment. The whole unit is furnished with     
necessary ventilation, lighting and fire-fighting system. There is air     
conditioners in the control compartment. 1.    
Technical     
Specification. 3.1 
Base load ( ISO condition ) ( guaranteed value )                                           
Distillate oil  Natural gas        
Output                   
kW          
40950       41890        
Heat rate           
          kJ/kW.h       
11342       11247     
        
Inlet temp. of turbine           
oC            
1140        
1140            
    
Exhaust temperature            
oC            
544         
546        
Exhaust gas flow            
kg/h x10x3            
526         
525        
Note:  above performance is     
measured at generator terminals and      
includes allowances for the effects on shaft driven auxiliaries, and         
2.55 in H2O ( 6.48 mbar ) inlet and 2.52 in H2O ( 6.4 mbar ) exhaust        
pressure drops and a NON DLN combustors.       
 3.2 
  Performance     
correction on the non-ISO conditions. 3.2.1 
Altitude correction on curve 416HA662 Rev A. 3.2.2 
Ambient temperature correction on curve 544HA876-2 Rev 0 and  544HA875-2Rev 
0. 3.2.3     
Effect of modulating IGV’s on exhaust temperature and flow on            
      
curve 544HA876-3Rev 0.and 544875-3 Rev.0 3.2.4 
Humidity correction on curve 498HA697 Rev B. 3.2.5 
Effect on pressure drop. l           
Air inlet     
pressure loss increase every 996 Pa, results an output         
decrease of 1.50%, and a heat rate increase of 0.50%, exhaust       
    
temperature increase 1.2 oC. l           
Exhaust     
pressure loss increase every 996 Pa, results an output decrease of 0.50%, and a     
heat rate increase of 0.50%, exhaust temperature increase of 1.2 oC. 3.2.6 
NOx emission          
168 ppmVD  for natural gas          
327 ppmVD  for distillate oil 3.2.7 
Noise          
93 dB (A) at 1m from each machine 3.4     
Generator          
Type:                               
QFR-38-2         
Output:                              
38000 kW       
Voltage:                              
10500 V         
Current:          
                    2611.8     
A         
Frequency:                            
50 Hz         
Power factor:                              
0.8         
Speed:                                
3000 rpm         
Efficiency:                            
97.7%         
Protection type:                
            IP     
44         
Synchronous reactance (saturated):             
247%         
Transient reactance (saturated):                
22%         
Sub-transient reactance (saturated):             
14.8%         
Negative sequence reactance (saturated):         
19%         
Short circuit ratio:      
                   ≥0.46         
Insulation class:                             
F         
Connection:                            
Y         
Cooling mode:                             
CACW         
Cooling temperature                         
32℃ Note: 
The output of generator can be matched with the gas turbine output requirement.       
 Attached     
Curves: 416HA662     
Rev.A  Altitude vs Atmospheric     
Pressure and Altitude vs                       
Correction Factor for Gas Turbine Output and Fuel                      
Consumption 544HA420     
Rev.0  Effect of Compressor Inlet     
Temperature on Output,                      
Heat Rate, Heat Consumption, Exhaust Flow and                      
Exhaust Temperature at Base Load 544HA421     
Rev.0  Effect of Inlet Guide Vane on     
Exhaust Flow and                     
 Temperature as a Function of Output and       
                 
Compressor Inlet Temperature 498HA697     
Rev.B  Correction to Output and heat     
Rate for Non-ISO                       
Specific Humidity Conditions | 
 
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