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Vortex generating flow passage design for increased film cooling effectivenessIt is an object of the invention to provide a film cooling apparatus of increased effectiveness and efficiency. In accordance with the invention, a cooling fluid is injected into a hot flowing gas through a passageway in a wall which contains and is subject to the hot gas. The passageway is slanted in a downstream direction at an acute angle to the wall. A cusp shape is provided in the passageway to generate vortices in the injected cooling fluid thereby reducing the energy extracted from the hot gas for that purpose. The cusp shape increases both film cooling effectiveness and wall area coverage. The cusp may be at either the downstream or upstream side of the passageway, the former substantially eliminating flow separation of the cooling fluid from the wall immediately downstream of the passageway.
Document ID
19850025120
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Papell, S. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
July 16, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-580419
Patent Number: NASA-CASE-LEW-14039-1
Patent Number: US-PATENT-4,529,358
Accession Number
85N33433
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-14039-1|US-PATENT-4,529,358
Patent Application
US-PATENT-APPL-SN-580419
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