A high thermal efficiency for an engine requires that a cycle capable of producing high efficiency is first chosen, and that components that can operate at high efficiencies are used. The choices made in both areas are discussed below. The "enabling " technology is a high-temperature, high-effectiveness (0.975) regenerator, with a low pressure drop. This requires only a low cycle pressure ratio (about 2.5:1) for optimum performance. The component efficiencies of compressors and turbines of low pressure ratio are intrinsically high. W.T.P.I. also divides this low pressure ratio among three compressor stages and three turbine stages. Doing so greatly reduces the kinetic energy that is usually lost from single stages, and thus substa...
The paper presents a theoretical analysis of three advanced gas turbine recuperative-cycles, that is...
An analysis was carried out for different thermodynamic cycles of power plants with air turbines. Va...
The paper presents a theoretical analysis of three advanced gas turbine recuperative-cycles, that is...
Regenerative gas turbine engine cycle is presented that yields higher cycle efficiencies than simple...
Analytical expressions for the turbine expansion ratio in the first stage (the high-pressure turbine...
The gas turbine has been around for over a century, providing power for a variety of applications. T...
A clean and safe energy is the greatest challenges in meeting the requirements of green environment....
A gas turbine installation (GTI) consists of 5 main parts: an input device, a compressor, a combusti...
The paper presents a thermodynamic cycle analysis for three turboshaft engines. The first cycle is a...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
The study of evaporatively-cooled cycles is of interest because of the prospect of enhanced efficien...
The paper presents a theoretical analysis of three advanced gas turbine recuperative-cycles, that is...
An analysis was carried out for different thermodynamic cycles of power plants with air turbines. Va...
The paper presents a theoretical analysis of three advanced gas turbine recuperative-cycles, that is...
Regenerative gas turbine engine cycle is presented that yields higher cycle efficiencies than simple...
Analytical expressions for the turbine expansion ratio in the first stage (the high-pressure turbine...
The gas turbine has been around for over a century, providing power for a variety of applications. T...
A clean and safe energy is the greatest challenges in meeting the requirements of green environment....
A gas turbine installation (GTI) consists of 5 main parts: an input device, a compressor, a combusti...
The paper presents a thermodynamic cycle analysis for three turboshaft engines. The first cycle is a...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
long time, leading to firing temperatures of over 1500°C within the next two decades. This paper inv...
The study of evaporatively-cooled cycles is of interest because of the prospect of enhanced efficien...
The paper presents a theoretical analysis of three advanced gas turbine recuperative-cycles, that is...
An analysis was carried out for different thermodynamic cycles of power plants with air turbines. Va...
The paper presents a theoretical analysis of three advanced gas turbine recuperative-cycles, that is...