NASA NTRS · 19790023036
Experimental Clean Combustor Program (ECCP), phase 3
Abstract
A double annular advanced technology combustor with low pollutant emission levels was evaluated in a series of CF6-50 engine tests. Engine lightoff was readily obtained and no difficulties were encountered with combustor staging. Engine acceleration and deceleration were smooth, responsive and essentially the same as those obtainable with the CF6-50 combustor. The emission reductions obtained in carbon monoxide, hydrocarbons, and nitrogen oxide levels were 55, 95, and 30 percent, respectively, at an idle power setting of 3.3 percent of takeoff power on an EPA parameter basis. Acceptable smoke levels were also obtained. The exit temperature distribution of the combustor was found to be its major performance deficiency. In all other important combustion system performance aspects, the combustor was found to be generally satisfactory.
Keep this discovery
Explore connections, maps & timelines
Gleason, C. C., Bahr, D. W.. 1979-06-01. Experimental Clean Combustor Program (ECCP), phase 3. https://ntrs.nasa.gov/citations/19790023036
Cite the original work for its findings. Save a collection to share your selection of sources.