Four combustion systems were designed and sized for the energy efficient engine. A fifth combustor was designed for the cycle and envelope of the twin-spool, high bypass ratio, high pressure ratio turbofan engine. Emission levels, combustion performance, life, and reliability assessments were made for these five combustion systems. Results of these design studies indicate that cruise NOx emission can be reduced by the use of lean, premixed-prevaporaized combustion and airflow modulation
The Lean Direct Injection (LDI) combustor is one of the low-emissions combustors with great potentia...
A Lean Premixed Prevaporized (LPP) low-emission combustor which is applied with the combustion techn...
International audienceCombustion engines in hybridized powertrains continue to require further reduc...
Phase 1 of the Lean Premixed-Prevaporized Comubstor Design Study is a nine month analytical study ef...
AbstractA key issue in the commercial aircraft engine design is environmental acceptability, and des...
Four combustor concepts, designed for the energy efficient engine, utilize variable geometry or othe...
Six conceptual combustor designs for the CF6-50 high bypass turbofan engine and six conceptual combu...
Lean Premixed Prevaporized (LPP) injection systems have been designed to offer a minimum NOx and soo...
Dry low Emissions (DLE) systems employing lean, premixed combustion have been successfully used with...
This chapter reviewed partially premixed and premixed aero engine combustors. Apart from a descripti...
Lean premixed prevaporized (LPP) combustion is a widely used concept for reducing pollutant emission...
The low-emissions combustor development described is directed toward advanced high pressure aircraft...
The low-emissions combustor development at the NASA Glenn Research Center is directed toward advance...
A lean-burn internally-staged combustor for low emissions that can be used in civil aviation gas tur...
Stringent emissions requirements for stationary gas turbines have produced new challenges in combust...
The Lean Direct Injection (LDI) combustor is one of the low-emissions combustors with great potentia...
A Lean Premixed Prevaporized (LPP) low-emission combustor which is applied with the combustion techn...
International audienceCombustion engines in hybridized powertrains continue to require further reduc...
Phase 1 of the Lean Premixed-Prevaporized Comubstor Design Study is a nine month analytical study ef...
AbstractA key issue in the commercial aircraft engine design is environmental acceptability, and des...
Four combustor concepts, designed for the energy efficient engine, utilize variable geometry or othe...
Six conceptual combustor designs for the CF6-50 high bypass turbofan engine and six conceptual combu...
Lean Premixed Prevaporized (LPP) injection systems have been designed to offer a minimum NOx and soo...
Dry low Emissions (DLE) systems employing lean, premixed combustion have been successfully used with...
This chapter reviewed partially premixed and premixed aero engine combustors. Apart from a descripti...
Lean premixed prevaporized (LPP) combustion is a widely used concept for reducing pollutant emission...
The low-emissions combustor development described is directed toward advanced high pressure aircraft...
The low-emissions combustor development at the NASA Glenn Research Center is directed toward advance...
A lean-burn internally-staged combustor for low emissions that can be used in civil aviation gas tur...
Stringent emissions requirements for stationary gas turbines have produced new challenges in combust...
The Lean Direct Injection (LDI) combustor is one of the low-emissions combustors with great potentia...
A Lean Premixed Prevaporized (LPP) low-emission combustor which is applied with the combustion techn...
International audienceCombustion engines in hybridized powertrains continue to require further reduc...