Experimental Clean Combustor Program: description and status
Conference
·
OSTI ID:7353506
The Experimental Clean Combustor Program is described. The program objectives include the generation and demonstration of technology for development of advanced commercial CTOL aircraft engines with lower exhaust emissions than current aircraft and the demonstration of this technology in full scale engines in 1976. The program is being conducted in three phases: (1) the screening of low pollutant combustors; (2) refinement of the best combustors; (3) and engine demonstration of the best combustors. Pollution goals are emission index values of 20 and 4 for carbon monoxide and unburned hydrocarbons, respectively, at engine idle conditions and an oxide of nitrogen emission index level of 10 at engine takeoff conditions. Pollution reduction approaches which are being investigated include multiple burning zone combustors, investigations of improved fuel distribution, and preparation and staging of combustor airflow. Phase I of the program is approximately 50 percent completed, and preliminary test results indicate that all combustor designs, with sufficient additional effort, appear capable of achieving the idle pollutant goals. Reduction of NO/sub x/ by 50 percent are presently possible, though further reductions are at the expense of increased combustion inefficiencies at both low and high power conditions.
- Research Organization:
- National Aeronautics and Space Administration, Cleveland, Ohio (USA). Lewis Research Center
- OSTI ID:
- 7353506
- Report Number(s):
- NASA-TM-X-71547
- Country of Publication:
- United States
- Language:
- English
Similar Records
Experimental clean combustor program, Phase 2. Final report
Experimental clean combustor program, alternate fuels addendum, phase 2. Final report
Emission response from extended length, variable geometry gas turbine combustor
Technical Report
·
Sun Aug 01 00:00:00 EDT 1976
·
OSTI ID:7116590
Experimental clean combustor program, alternate fuels addendum, phase 2. Final report
Technical Report
·
Wed Dec 31 23:00:00 EST 1975
·
OSTI ID:7318528
Emission response from extended length, variable geometry gas turbine combustor
Conference
·
Mon Dec 31 23:00:00 EST 1973
·
OSTI ID:7357235
Related Subjects
33 ADVANCED PROPULSION SYSTEMS
330603 -- Vehicle Design Factors-- Engine System
330701* -- Emission Control-- Nitrogen Oxides
330702 -- Emission Control-- Carbon Monoxide
330704 -- Emission Control-- Hydrocarbons
AIRCRAFT
CARBON COMPOUNDS
CARBON MONOXIDE
CARBON OXIDES
CHALCOGENIDES
COMBUSTION CHAMBERS
DESIGN
ENGINES
EXHAUST GASES
FUEL SYSTEMS
GASEOUS WASTES
HYDROCARBONS
INTERNAL COMBUSTION ENGINES
NITROGEN COMPOUNDS
NITROGEN OXIDES
ORGANIC COMPOUNDS
OXIDES
OXYGEN COMPOUNDS
RESEARCH PROGRAMS
WASTES
330603 -- Vehicle Design Factors-- Engine System
330701* -- Emission Control-- Nitrogen Oxides
330702 -- Emission Control-- Carbon Monoxide
330704 -- Emission Control-- Hydrocarbons
AIRCRAFT
CARBON COMPOUNDS
CARBON MONOXIDE
CARBON OXIDES
CHALCOGENIDES
COMBUSTION CHAMBERS
DESIGN
ENGINES
EXHAUST GASES
FUEL SYSTEMS
GASEOUS WASTES
HYDROCARBONS
INTERNAL COMBUSTION ENGINES
NITROGEN COMPOUNDS
NITROGEN OXIDES
ORGANIC COMPOUNDS
OXIDES
OXYGEN COMPOUNDS
RESEARCH PROGRAMS
WASTES