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Rotating stall suppressionRotating stall in an axial-flow compressor is suppressed by the positioning of a fixed inlet flow divider in the annular inlet flow passage upstream of the compressor. The inlet flow divider is aligned with the flow of fluid through the duct and acts to block or interfere with any rotating wave in the inlet and thereby suppresses rotating stall in the compressor.
Document ID
20080004001
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Moore, Franklin K.
Date Acquired
August 24, 2013
Publication Date
March 29, 1994
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-815028
Patent Number: US-PATENT-5,297,930
Funding Number(s)
CONTRACT_GRANT: NAG3-349
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,297,930
Patent Application
US-PATENT-APPL-SN-815028
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