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Flame Tube NOx Emissions Using a Lean-Direct-Wall-Injection Combustor ConceptA low-NOx emissions combustor concept has been demonstrated in flame tube tests. A lean-direct injection concept was used where the fuel is injected directly into the flame zone and the overall fuel-air mixture is lean. In this concept the air is swirled upstream of a venturi section and the fuel is injected radially inward into the air stream from the throat section using a plain-orifice injector. Configurations have two-, four-, or six-wall fuel injectors and in some cases fuel is also injected from an axially located simplex pressure atomizer. Various orifice sizes of the plain-orifice injector were evaluated for the effect on NOx. Test conditions were inlet temperatures up to 8 1 OK, inlet pressures up to 2760 kPa, and flame temperatures up to 2100 K. A correlation is developed relating the NOx emissions to inlet temperature, inlet pressure, fuel-air ratio and pressure drop. Assuming that 15 percent of the combustion air would be used for liner cooling and using an advanced engine cycle, for the best configuration, the NOx emissions using the correlation is estimated to be <75 percent of the 1996 ICAO standard.
Document ID
20020014404
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Tacina, Robert R.
(NASA Glenn Research Center Cleveland, OH United States)
Wey, Changlie
(QSS Group, Inc. Brook Park, OH United States)
Choi, Kyung J.
(Drexel Univ. Philadelphia, PA United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2001
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:211105
E-12950
NASA/TM-2001-21105
AIAA Paper 2001-3271
Report Number: NAS 1.15:211105
Report Number: E-12950
Report Number: NASA/TM-2001-21105
Report Number: AIAA Paper 2001-3271
Meeting Information
Meeting: 37th Joint Propulsion Conference and Exhibit
Location: Salt Lake City, UT
Country: United States
Start Date: July 8, 2001
End Date: July 11, 2001
Sponsors: American Society for Engineering Education, American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc.
Funding Number(s)
PROJECT: RTOP 708-28-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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