NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Emissions Measurements from a Lobed Fuel Injector/BurnerThe present experimental study examines NO(x) and CO emissions associated with alternative fuel injector geometries. These injectors mix fuel and air to differing extents and thus create different local equivalence ratios upstream of flame ignition and stabilization. Two of the devices studied are lobed fuel injectors, in which mixing of reactants is associated with stream wise vorticity generation and straining of fuel-air interfaces, while the third is a non-lobed fuel injector which creates relatively little fuel-air mixing prior to ignition.Results show that one lobed injector geometry appears to produce locally lean premixed flame structures, resulting in low NO. emissions when compared with non-lobed injector emissions. The other lobed injector geometry appears to produce a local fuel-air mixture which is closer to stoichiometric conditions, with NO(x) emissions that are actually higher than for the non-lobed injector. For both lobed injector geometries examined here, CO emissions become high for over-all lean operating conditions, consistent with premixed combustion behavior. The present study demonstrates the importance of control of the local equivalence ratio in minimizing burner emissions.
Document ID
19990062145
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Mitchell, M. G.
(California Univ. Los Angeles, CA United States)
Smith, L. L.
(California Univ. Los Angeles, CA United States)
Karagozian, A. R.
(California Univ. Los Angeles, CA United States)
Smith, O. I.
(California Univ. Los Angeles, CA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1998
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
AIAA Paper 98-0802
Meeting Information
Meeting: Aerospace Sciences
Location: Reno, NV
Country: United States
Start Date: January 12, 1998
End Date: January 15, 1998
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NCC2-374
CONTRACT_GRANT: N00014-93-1-1383
CONTRACT_GRANT: NASA Order H-2358
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available