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Effect of flame-tube head structure on combustion chamber performanceThe experimental combustion performance of a premixed, pilot-type flame tube with various head structures is discussed. The test study covers an extensive area: efficiency of the combustion chamber, quality of the outlet temperature field, limit of the fuel-lean blowout, ignition performance at ground starting, and carbon deposition. As a result of these tests, a nozzle was found which fits the premixed pilot flame tube well. The use of this nozzle optimized the performance of the combustion chamber. The tested models had premixed pilot chambers with two types of air-film-cooling structures, six types of venturi-tube structures, and secondary fuel nozzles with two small spray-cone angles.
Document ID
19870010842
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gu, Minqqi
(Shenyang Aeroengine Research Inst.)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Publication Information
Publication: NASA- Lewis Research Center NASA-Chinese Aeronautical Establishment (CAE) Symposium
Subject Category
Aircraft Propulsion And Power
Accession Number
87N20275
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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