NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design and evaluation of combustors for reducing aircraft engine pollutionVarious techniques and test results are briefly described and referenced for detail. The effort arises from the increasing concern for the measurement and control of emissions from gas turbine engines. The greater part of this research is focused on reducing the oxides of nitrogen formed during takeoff and cruise in both advanced CTOL, high pressure ratio engines, and advanced supersonic aircraft engines. The experimental approaches taken to reduce oxides of nitrogen emissions include the use of: multizone combustors incorporating reduced dwell time, fuel-air premixing, air atomization, fuel prevaporization, water injection, and gaseous fuels. In the experiments conducted to date, some of these techniques were more successful than others in reducing oxides of nitrogen emissions. Tests are being conducted on full-annular combustors at pressures up to 6 atmospheres and on combustor segments at pressures up to 30 atmospheres.
Document ID
19740006189
Document Type
Conference Paper
Authors
Jones, R. E. (NASA Lewis Research Center Cleveland, OH, United States)
Grobman, J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 7, 2013
Publication Date
September 1, 1973
Publication Information
Publication: AGARD Atmospheric Pollution by Aircraft Engine
Subject Category
PROPULSION SYSTEMS
Distribution Limits
Public
Copyright
Other
Document Inquiry