This paper presents a demonstration of a novel lean premixed low-swirl injector (LSI) concept for ultra-low NOx gas turbines. Low-swirl flame stabilization method is a recent discovery that is being applied to atmospheric heating equipment. Low-swirl burners are simple and support ultra-lean premixed flames that are less susceptible to combustion instabilities than conventional high-swirl designs. As a first step towards transferring this method to turbines, an injector modeled after the design of atmospheric low-swirl burner has been tested up to T=646 F and 10 atm and shows good promise for future development
A need exists to develop and demonstrate a low pollutant emission gas turbine combustor design that ...
A low-NO (sub x) aircraft gas turbine engine combustion concept was developed and tested. The concep...
Contents Introduction Thermal NOx Burning to the lean flammability limit for successful ultra low NO...
This paper describes the continuing development of the Weak-Swirl Burner (WSB) for use in low NOx a...
This paper describes the continuing development of the weak-swirl burner (WSB) for use in low NO{sub...
Industrial gas turbines are primarily fueled with natural gas. However, changes in fuel cost and ava...
Laboratory experiments have been conducted to investigate the fuel effects on the turbulent premixed...
Alzeta Corporation has developed surface-stabilized fuel injectors for use with lean premixed combus...
Laboratory experiments were conducted at gas turbine and atmospheric conditions (0.101 < P{sub 0}...
This paper summarizes research on the lean direct injection (LDI) combustor concept for aero-gas tur...
This study was motivated by recent tests results showing that a 5cm i.d. low-swirl burner (LSB) sta...
The low-emissions combustor development at the NASA Glenn Research Center is directed toward advance...
Clean gas turbine combustion research has gained popularity in power generation and propulsion indus...
The combustion of fossil fuels remains a key technology as these fuels are the main source of energy...
This paper first highlights recent developments in lean direct injection (LDI) combustion technology...
A need exists to develop and demonstrate a low pollutant emission gas turbine combustor design that ...
A low-NO (sub x) aircraft gas turbine engine combustion concept was developed and tested. The concep...
Contents Introduction Thermal NOx Burning to the lean flammability limit for successful ultra low NO...
This paper describes the continuing development of the Weak-Swirl Burner (WSB) for use in low NOx a...
This paper describes the continuing development of the weak-swirl burner (WSB) for use in low NO{sub...
Industrial gas turbines are primarily fueled with natural gas. However, changes in fuel cost and ava...
Laboratory experiments have been conducted to investigate the fuel effects on the turbulent premixed...
Alzeta Corporation has developed surface-stabilized fuel injectors for use with lean premixed combus...
Laboratory experiments were conducted at gas turbine and atmospheric conditions (0.101 < P{sub 0}...
This paper summarizes research on the lean direct injection (LDI) combustor concept for aero-gas tur...
This study was motivated by recent tests results showing that a 5cm i.d. low-swirl burner (LSB) sta...
The low-emissions combustor development at the NASA Glenn Research Center is directed toward advance...
Clean gas turbine combustion research has gained popularity in power generation and propulsion indus...
The combustion of fossil fuels remains a key technology as these fuels are the main source of energy...
This paper first highlights recent developments in lean direct injection (LDI) combustion technology...
A need exists to develop and demonstrate a low pollutant emission gas turbine combustor design that ...
A low-NO (sub x) aircraft gas turbine engine combustion concept was developed and tested. The concep...
Contents Introduction Thermal NOx Burning to the lean flammability limit for successful ultra low NO...