Six catalytic combustor concepts were defined, analyzed, and evaluated. Major design considerations included low emissions, performance, safety, durability, installations, operations and development. On the basis of these considerations the two most promising concepts were selected. Refined analysis and preliminary design work was conducted on these two concepts. The selected concepts were required to fit within the combustor chamber dimensions of the reference engine. This is achieved by using a dump diffuser discharging into a plenum chamber between the compressor discharge and the turbine inlet, with the combustors overlaying the prediffuser and the rear of the compressor. To enhance maintainability, the outer combustor case for each con...
Three advanced combustor concepts, designed for the AiResearch TFE 731-2 turbofan engine, were evalu...
The aim of this four year project which started in November 1992, was to research novel catalytic co...
The low-emissions combustor development described is directed toward advanced high pressure aircraft...
The feasibility of employing the known attractive and distinguishing features of catalytic combustio...
An overview of the ongoing program is presented. Objectives, plan, schedule, pollution and performan...
The Advanced Low Emissions Catalytic Combustors Program (ALECC) is being undertaken to evaluate the ...
Several combustor concepts were designed and tested to demonstrate significant reductions in aircraf...
Four combustor concepts, designed for the energy efficient engine, utilize variable geometry or othe...
A gas turbine technology program to improve and optimize the staged rich lean low NOx combustor conc...
Full annular versions of advanced combustor designs, sized to fit within the CF6-50 engine, were def...
Phase 1 of the Lean Premixed-Prevaporized Comubstor Design Study is a nine month analytical study ef...
A total of twelve low NOx combustor configurations, embodying three different combustion concepts, w...
Fuel injectors to provide a premixed prevaporized fuel-air mixture are studied. An evaluation of com...
The generation of technology was studied for the development of advanced commercial CTOL aircraft en...
A combustor program was conducted to evolve and to identify the technology needed for, and to establ...
Three advanced combustor concepts, designed for the AiResearch TFE 731-2 turbofan engine, were evalu...
The aim of this four year project which started in November 1992, was to research novel catalytic co...
The low-emissions combustor development described is directed toward advanced high pressure aircraft...
The feasibility of employing the known attractive and distinguishing features of catalytic combustio...
An overview of the ongoing program is presented. Objectives, plan, schedule, pollution and performan...
The Advanced Low Emissions Catalytic Combustors Program (ALECC) is being undertaken to evaluate the ...
Several combustor concepts were designed and tested to demonstrate significant reductions in aircraf...
Four combustor concepts, designed for the energy efficient engine, utilize variable geometry or othe...
A gas turbine technology program to improve and optimize the staged rich lean low NOx combustor conc...
Full annular versions of advanced combustor designs, sized to fit within the CF6-50 engine, were def...
Phase 1 of the Lean Premixed-Prevaporized Comubstor Design Study is a nine month analytical study ef...
A total of twelve low NOx combustor configurations, embodying three different combustion concepts, w...
Fuel injectors to provide a premixed prevaporized fuel-air mixture are studied. An evaluation of com...
The generation of technology was studied for the development of advanced commercial CTOL aircraft en...
A combustor program was conducted to evolve and to identify the technology needed for, and to establ...
Three advanced combustor concepts, designed for the AiResearch TFE 731-2 turbofan engine, were evalu...
The aim of this four year project which started in November 1992, was to research novel catalytic co...
The low-emissions combustor development described is directed toward advanced high pressure aircraft...