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Effects of fuel-injector design on ultra-lean combustion performanceEmissions data were obtained for six fuel injector configurations tested with ultra lean combustion. Fuel injectors included three multiple source designs and three configurations using a single air assist injector. Only the multiple source fuel injectors provided acceptable emissions. Values of 16g CO/kg fuel, 1.9g HC/kg fuel, and 19.g NO2/kg fuel were obtained for the combustion temperature range of 1450 to 1700 K for both a high blockage 19 source injector and a low blockage 41 source injector. It was shown that high fuel injector pressure drop may not be required to achieve low emissions performance at high inlet air temperature when the fuel is well dispersed in the airstream.
Document ID
19810015998
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, D. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Energy Production And Conversion
Report/Patent Number
DOE/NASA/51040-26
E-877
NASA-TM-82624
Report Number: DOE/NASA/51040-26
Report Number: E-877
Report Number: NASA-TM-82624
Meeting Information
Meeting: Intersoc. Energy Conversion Eng. Conf.,
Location: Atlanta, GA
Country: United States
Start Date: August 9, 1981
End Date: August 14, 1981
Accession Number
81N24533
Funding Number(s)
CONTRACT_GRANT: DE-A101-77CS-51040
PROJECT: RTOP 778-32-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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