AbstractA key issue in the commercial aircraft engine design is environmental acceptability, and designers are continually challenged to reduce emissions. In this paper, an experimental investigation is performed to evaluate the emission performance of a liquid-fueled trapped vortex combustor (TVC) under lean premixed prevaporized (LPP) mode. When operating as an LPP system, a TVC is fueled both in the cavities and in the main stream. The correlations between the emission performance and the total excess air ratio, the positions (4 positions) of the fuel injectors in the main stream, and the inlet temperature are obtained. Experimental results show that both the volume concentrations of unburnt hydrocarbon (UHC) and NOx (NO, NO2 usually gro...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions.This...
AbstractThe foundation of AVIC Commercial Aircraft Engine Company (ACAE) in Shanghai triggers the ho...
This paper presents experimental results for a low-NOxaero gas turbine combustor, in particular, a t...
AbstractA key issue in the commercial aircraft engine design is environmental acceptability, and des...
AbstractA trapped vortex combustor (TVC) has been a very promising novel concept for it offers impro...
This paper summarizes the development of lean direct injection (LDI) combustor technology at, or in ...
The low-emissions combustor development at the NASA Glenn Research Center is directed toward advance...
A Lean Premixed Prevaporized (LPP) low-emission combustor which is applied with the combustion techn...
An experimental and computational study was conducted to evaluate the performance and emissions char...
A low-NO (sub x) aircraft gas turbine engine combustion concept was developed and tested. The concep...
The low-emissions combustor development described is directed toward advanced high pressure aircraft...
AbstractA lean-burn internally-staged combustor for low emissions that can be used in civil aviation...
Effects of fuel vaporization on the exhaust emission levels of oxides of nitrogen (NOX), carbon mono...
Three variations of a low emissions aircraft gas turbine engine combustion concept were developed an...
Several combustor concepts were designed and tested to demonstrate significant reductions in aircraf...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions.This...
AbstractThe foundation of AVIC Commercial Aircraft Engine Company (ACAE) in Shanghai triggers the ho...
This paper presents experimental results for a low-NOxaero gas turbine combustor, in particular, a t...
AbstractA key issue in the commercial aircraft engine design is environmental acceptability, and des...
AbstractA trapped vortex combustor (TVC) has been a very promising novel concept for it offers impro...
This paper summarizes the development of lean direct injection (LDI) combustor technology at, or in ...
The low-emissions combustor development at the NASA Glenn Research Center is directed toward advance...
A Lean Premixed Prevaporized (LPP) low-emission combustor which is applied with the combustion techn...
An experimental and computational study was conducted to evaluate the performance and emissions char...
A low-NO (sub x) aircraft gas turbine engine combustion concept was developed and tested. The concep...
The low-emissions combustor development described is directed toward advanced high pressure aircraft...
AbstractA lean-burn internally-staged combustor for low emissions that can be used in civil aviation...
Effects of fuel vaporization on the exhaust emission levels of oxides of nitrogen (NOX), carbon mono...
Three variations of a low emissions aircraft gas turbine engine combustion concept were developed an...
Several combustor concepts were designed and tested to demonstrate significant reductions in aircraf...
Lean Direct Injection (LDI) is a combustor concept that reduces nitrogen oxides (NOx) emissions.This...
AbstractThe foundation of AVIC Commercial Aircraft Engine Company (ACAE) in Shanghai triggers the ho...
This paper presents experimental results for a low-NOxaero gas turbine combustor, in particular, a t...