1979
DOI: 10.2514/3.62408
|View full text |Cite
|
Sign up to set email alerts
|

Combustor Concepts for Aircraft Gas Turbine Low-Power Emissions Reduction

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
2
0

Year Published

1989
1989
2021
2021

Publication Types

Select...
2
1

Relationship

0
3

Authors

Journals

citations
Cited by 3 publications
(2 citation statements)
references
References 1 publication
0
2
0
Order By: Relevance
“…Thus, in continuous flow combustors burning liquid fuels, more NO is formed than would be expected from calculations of adiabatic flame temperatures based on the overall fuel/air ratio in the combustion zone. For these reasons, technology for the control and reduction of NO emissions from gas turbine combustors have tended to focus on means for reducing flame temperatures and eliminating fuel droplet combustion (Mularz et al, 1979, and Bahr, 1972, 1973.…”
Section: Introductionmentioning
confidence: 99%
“…Thus, in continuous flow combustors burning liquid fuels, more NO is formed than would be expected from calculations of adiabatic flame temperatures based on the overall fuel/air ratio in the combustion zone. For these reasons, technology for the control and reduction of NO emissions from gas turbine combustors have tended to focus on means for reducing flame temperatures and eliminating fuel droplet combustion (Mularz et al, 1979, and Bahr, 1972, 1973.…”
Section: Introductionmentioning
confidence: 99%
“…When the combustion efficiency decreases, the concentrations of carbon monoxide and unburned fuel increase. Therefore, air-assisted fuel nozzles have been applied to generate fine droplets [6,8], and catalysts have been used in injection systems [9].…”
Section: Introductionmentioning
confidence: 99%