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Swirl can primary combustorA swirl can full annulus combustor, operable over a wide range of exit average temperatures is used in a high performance gas turbine engine for advanced aircraft. A large number of swirl can modules are mounted in an array in each combustor.
Document ID
19730021933
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Jones, R. E. (NASA Lewis Research Center Cleveland, OH, United States)
Niedzwiecki, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 31, 1973
Subject Category
Physics, General
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-192970
Patent Number: NASA-CASE-LEW-11326-1
Patent Number: US-PATENT-3,748,853
Accession Number
73N30665
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-11326-1|US-PATENT-3,748,853
Patent Application
US-PATENT-APPL-SN-192970

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