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Swirl-can combustor segmentCombustor produces uniform circumferential and radial combustor exit temperature profiles and high combustion efficiency at high temperature loads. Absence of diluent air entry ports eliminates stress concentration points, low pressure fuel alleviates nozzle fouling, and abundant air at all burning stages reduces smoke.
Document ID
19700000310
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Jones, R.
Moyer, H.
Niedzwiecki, R.
Date Acquired
August 5, 2013
Publication Date
June 1, 1970
Subject Category
Machinery
Report/Patent Number
LEW-11082
Report Number: LEW-11082
Accession Number
70B10322
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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