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Gas turbine combustor PatentMethod for maintaining good performance in gas turbine during air flow distortion
Document ID
19710019439
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Authors
Humenik, F. M. (NASA Lewis Research Center Cleveland, OH, United States)
Norgren, C. T. (NASA Lewis Research Center Cleveland, OH, United States)
Roudebush, W. H. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-839994
Patent Number: US-PATENT-3,581,492
Patent Number: NASA-CASE-LEW-10286-1
Accession Number
71N28915
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,581,492|NASA-CASE-LEW-10286-1
Patent Application
US-PATENT-APPL-SN-839994

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