Theoretical and Experimental Analysis of Heavy Duty Gas Turbine Performance Depending on Ambient Conditions

2003 ◽  
Author(s):  
S. Brusca ◽  
R. Lanzafame
Keyword(s):  
Mathematical Model ◽  
Gas Turbine ◽  
Thermodynamic Analysis ◽  
Engine Performance ◽  
Fuel Oil ◽  
Engine Control ◽  
Heavy Duty ◽  
Ambient Conditions ◽  
Control Logic ◽  
Heavy Duty Gas Turbine

A mathematical model of a heavy duty gas turbine has been implemented using GateCycle™ code. This model is able to simulate the engine behavior running on syngas and fuel oil. Also engine control logic is implemented using Microsoft Excel™ VBA language. The model implemented has been finely tuned and tested with measured data. Test results show that it is able to simulate engine running in on-design and off-design conditions. Using this model, an extensive thermodynamic analysis of light fuel oil and syngas fed engine performance has been carried out in respect of ambient conditions. As it is possible to see in the results of the thermodynamic analysis, at high air temperatures performance reduction occur. Relative humidity have a slightly effect on engine performance when the latter is running on syngas. Instead it doesn’t have a relevant effect on the performance of the engine running on light liquid fuel oil in all the range of ambient temperature investigated. Results of this analysis also show the correct replication of the engine control system. In conclusion, the developed mathematical model is able to simulate gas turbine operations with low errors. So that, it could be used in order to optimise engine performance at the ambient conditions that occur for the site of the IGCC Complex in which gas turbine has integrated as topper.

scholarly journals Heavy-Duty Gas Turbine Plant Aerothermodynamic Simulation Using Simulink

1996 ◽  
Author(s):  
G. Crosa ◽  
F. Pittaluga ◽  
A. Trucco Martinengo ◽  
F. Beltrami ◽  
A. Torelli ◽  
...  
Keyword(s):  
Mathematical Model ◽  
Gas Turbine ◽  
Dynamic Responses ◽  
State Variables ◽  
Algebraic Equations ◽  
Heavy Duty ◽  
Combustion Chambers ◽  
Turbine Plant ◽  
Gas Turbine Plant ◽  
Heavy Duty Gas Turbine

This paper presents a physical simulator for predicting the off-design and dynamic behaviour of a single shaft heavy-duty gas turbine plant, suitable for gas-steam combined cycles. The mathematical model, which is non linear and based on the lumped parameter approach, is described by a set of first-order differential and algebraic equations. The plant components are described adding to their steady state characteristics the dynamic equations of mass, momentum and energy balances. The state variables are mass flow rates, static pressures, static temperatures of the fluid, wall temperatures and shaft rotational speed. The analysis has been applied to a 65 MW heavy-duty gas turbine plant with two off-board silo-type combustion chambers. To model the compressor, equipped with variable inlet guide vanes, a subdivision into five partial compressors is adopted, in serial arrangement, separated by dynamic blocks. The turbine is described using a one dimensional row by row mathematical model, that takes into account both the air bleed cooling effect and the mass storage among the stages. The simulation model considers also the air bleed transformations from the compressor down to the turbine. Both combustion chambers have been modelled utilising a sequence of several sub-volumes, to simulate primary and secondary zones in presence of three hybrid burners. A code has been created in Simulink environment. Some dynamic responses of the simulated plant, equipped with a proportional-integral speed regulator, are presented.

Analysis of Singas FED Gas Turbine Performance Depending on Ambient Conditions

2003 ◽  
Author(s):  
S. Brusca ◽  
R. Lanzafame
Keyword(s):  
Mathematical Model ◽  
Relative Humidity ◽  
Gas Turbine ◽  
Engine Performance ◽  
Maximum Relative Error ◽  
Ambient Conditions ◽  
Turbine Performance ◽  
Air Temperatures ◽  
Performance Reduction ◽  
Relative Errors

It is well known that gas turbine performance is quite influenced by ambient conditions such as pressure, air temperature and relative humidity. This paper deals with the effects of ambient conditions on performance of gas turbine fired with syngas. A mathematical model of the engine has been implemented within GateCycle workspace and using experimental data, it has been finely tuned and tested. Results analysis showed that it is able to simulate engine running in on–design and off–design conditions (maximum relative error is about 1%). Thus, gas turbine running simulations depending on ambient temperature and relative humidity have been carried out. Results analysis showed that at high air temperatures (higher then the one corresponding to maximum IGV opening) performance reduction occur. On the contrary, high values of relative humidity allow to reduce power losses in the same temperature range. In conclusion, the developed mathematical model is able to simulate gas turbine running with low relative errors. So that, it could be used in order to optimise engine performance at the ambient conditions that occur for the site of the IGCC Complex in which gas turbine is integrated.

Heavy-Duty Gas Turbine Plant Aerothermodynamic Simulation Using Simulink

1998 ◽  
Vol 120 (3) ◽  
pp. 550-556 ◽  
Author(s):  
G. Crosa ◽  
F. Pittaluga ◽  
A. Trucco ◽  
F. Beltrami ◽  
A. Torelli ◽  
...  
Keyword(s):  
Mathematical Model ◽  
Gas Turbine ◽  
Dynamic Responses ◽  
State Variables ◽  
Algebraic Equations ◽  
Heavy Duty ◽  
Combustion Chambers ◽  
Turbine Plant ◽  
Gas Turbine Plant ◽  
Heavy Duty Gas Turbine

This paper presents a physical simulator for predicting the off-design and dynamic behavior of a single shaft heavy-duty gas turbine plant, suitable for gas-steam combined cycles. The mathematical model, which is nonlinear and based on the lumped parameter approach, is described by a set of first-order differential and algebraic equations. The plant components are described adding to their steady-state characteristics the dynamic equations of mass, momentum, and energy balances. The state variables are mass flow rates, static pressures, static temperatures of the fluid, wall temperatures, and shaft rotational speed. The analysis has been applied to a 65 MW heavy-duty gas turbine plant with two off-board, silo-type combustion chambers. To model the compressor, equipped with variable inlet guide vanes, a subdivision into five partial compressors is adopted, in serial arrangement, separated by dynamic blocks. The turbine is described using a one-dimensional, row-by-row mathematical model, that takes into account both the air bleed cooling effect and the mass storage among the stages. The simulation model considers also the air bleed transformations from the compressor down to the turbine. Both combustion chambers have been modeled utilizing a sequence of several sub-volumes, to simulate primary and secondary zones in presence of three hybrid burners. A code has been created in Simulink environment. Some dynamic responses of the simulated plant, equipped with a proportional-integral speed regulator, are presented.

A New Superalloy Enabling Heavy Duty Gas Turbine Wheels for Improved Combined Cycle Efficiency

2017 ◽  
Author(s):  
Andrew Detor ◽  
◽  
Richard DiDomizio ◽  
Don McAllister ◽  
Erica Sampson ◽  
...  
Keyword(s):  
Gas Turbine ◽  
Combined Cycle ◽  
Heavy Duty ◽  
Heavy Duty Gas Turbine ◽  
Cycle Efficiency

Impact of Different Film-Cooling Modes at Trailing Edge on the Aerodynamic Performance of Heavy Duty Gas Turbine Cascade

2011 ◽  
Vol 84-85 ◽  
pp. 259-263
Author(s):  
Xun Liu ◽  
Song Tao Wang ◽  
Xun Zhou ◽  
Guo Tai Feng
Keyword(s):  
Gas Turbine ◽  
Film Cooling ◽  
Large Mass ◽  
Turbine Cascade ◽  
Heavy Duty ◽  
Trailing Edge ◽  
Central Difference ◽  
Adiabatic Effectiveness ◽  
Heavy Duty Gas Turbine ◽  
The Impact

In this paper, the trailing edge film cooling flow field of a heavy duty gas turbine cascade has been studied by central difference scheme and multi-block grid technique. The research is based on the three-dimensional N-S equation solver. By way of analysis of the temperature field, the distribution of profile pressure, and the distribution of film-cooling adiabatic effectiveness in the region of trailing edge with different cool air injection mass and different angles, it is found that the impact on the film-cooling adiabatic effectiveness is slightly by changing the injection mass. The distribution of profile pressure dropped intensely at the pressure side near the injection holes line with the large mass cooling air. The cooling effect is good in the region of trailing edge while the injection air is along the direction of stream.

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