In this work the thermoeconomic features of two different combined cycles using air "open loop" and steam "closed loop" cooled gas turbines are presented and compared in depth. In order to properly estimate both thermodynamic and thermoeconomic performance of the different combined cycles an analytical model of the blade cooling system has been developed in details and outlined in the paper. Internal Thermoeconomic functional analysis is not performed here, as only economic results are shown and discussed. The blade cooling detailed model, originally developed by TPG researchers, has been integrated into the web based modular code WTEMP, already validated for GT based cycles, developed in the last ten years by TPG. It is shown that the clos...
Cooling is essential in all modern high-temperature gas turbines. Turbine cooling is mainly a functi...
The objective of this thesis is to determine if an advanced gas turbine cycle exists, which can c...
In order to capture the behaviour of the oxyfuel cycle operating with high combustor-outlet temperat...
All major manufacturers of large size gas turbines are developing new techniques aimed at achieving ...
A method for simulating the cooled gas turbine is demonstrated. Based on equations and other knowled...
A thermodynamic and economic analysis of a GT10 gas turbine integrated with the air bottoming cycle ...
A triple pressure combined gas turbine cycle reference plant is established targeting technology tha...
Gas turbine (GT) power plants operating in arid climates suffer a decrease in output power during th...
The combined cycle gas-turbine (CCGT) power plant is a highly developed technology which generates e...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
This paper reports on a techno-economical parametric analysis of an inlet air cooling system applied...
The growth of cogeneration technology has accelerated in recent years, and it is estimated that fift...
This paper discusses the thermodynamics of power cycles where steam or water are mixed with air (or ...
Turbine Inlet Temperatures of 1500-2000K have become a sort of standard for most modern advanced app...
A predicting model of cooling air percentage for turbine blades with respect to simple-cycle triple...
Cooling is essential in all modern high-temperature gas turbines. Turbine cooling is mainly a functi...
The objective of this thesis is to determine if an advanced gas turbine cycle exists, which can c...
In order to capture the behaviour of the oxyfuel cycle operating with high combustor-outlet temperat...
All major manufacturers of large size gas turbines are developing new techniques aimed at achieving ...
A method for simulating the cooled gas turbine is demonstrated. Based on equations and other knowled...
A thermodynamic and economic analysis of a GT10 gas turbine integrated with the air bottoming cycle ...
A triple pressure combined gas turbine cycle reference plant is established targeting technology tha...
Gas turbine (GT) power plants operating in arid climates suffer a decrease in output power during th...
The combined cycle gas-turbine (CCGT) power plant is a highly developed technology which generates e...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
This paper reports on a techno-economical parametric analysis of an inlet air cooling system applied...
The growth of cogeneration technology has accelerated in recent years, and it is estimated that fift...
This paper discusses the thermodynamics of power cycles where steam or water are mixed with air (or ...
Turbine Inlet Temperatures of 1500-2000K have become a sort of standard for most modern advanced app...
A predicting model of cooling air percentage for turbine blades with respect to simple-cycle triple...
Cooling is essential in all modern high-temperature gas turbines. Turbine cooling is mainly a functi...
The objective of this thesis is to determine if an advanced gas turbine cycle exists, which can c...
In order to capture the behaviour of the oxyfuel cycle operating with high combustor-outlet temperat...