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Combustor flame flashback

Authors :
Proctor, M. P
Anderson, D. N
Tien, J. S
Source :
Combust. Fundamentals Res..
Publication Year :
1984
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1984.

Abstract

Flashback, a problem that occurs in premixed-prevaporized combustors, is the upstream propagation of the flame from the combustor into the premixing tubes. Not only does flashback change the combustion process from premixed burning to diffusion burning, thus creating more pollutants, but it also inflicts considerable damage to the fuel injector, premixing tube and other equipment upstream. The conditions at which flashback occurs in steady burning and the mechanism that causes flashback in both steady and transient flow are studied. The equivalence ratio at which flashback occurs is being measured for inlet temperatures of 600-950 K, premixer wall temperatures of 450-1050 K and premixer velocities of 40-80 ft/s. These data are presented.

Subjects

Subjects :
Inorganic And Physical Chemistry

Details

Language :
English
Database :
NASA Technical Reports
Journal :
Combust. Fundamentals Res.
Publication Type :
Report
Accession number :
edsnas.19840012493
Document Type :
Report