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Effect of broad properties fuel on injector performance in a reverse flow combustorThe effect of fuel type on the performance of various fuel injectors was investigated in a reverse flow combustor. Combustor performance and emissions are documented for simplex pressure atomizing, spill flow, and airblast fuel injectors using a broad properties fuel and compared with performance using Jet A fuel. Test conditions simulated a range of flight conditions including sea level take off, low and high altitude cruise, as well as a parametric evaluation of the effect of increased combustor loading. The baseline simplex injector produced higher emission levels with corresponding lower combustion efficiency with the broad properties fuel. There was little or not loss in performance by the two advanced concept injectors with the broad properties fuel. The airblast injector proved to be especially insensitive to fuel type.
Document ID
19830004831
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Raddlebaugh, S. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Norgren, C. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-1448
NASA-TM-83013
AIAA PAPER 83-0154
NAS 1.15:83013
Report Number: E-1448
Report Number: NASA-TM-83013
Report Number: AIAA PAPER 83-0154
Report Number: NAS 1.15:83013
Meeting Information
Meeting: Aerospace Sci. Conf.
Location: Reno, NV
Country: United States
Start Date: January 10, 1983
End Date: January 13, 1983
Sponsors: AIAA
Accession Number
83N13101
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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