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Segmented trapped vortex cavityAn annular trapped vortex cavity assembly segment comprising includes a cavity forward wall, a cavity aft wall, and a cavity radially outer wall there between defining a cavity segment therein. A cavity opening extends between the forward and aft walls at a radially inner end of the assembly segment. Radially spaced apart pluralities of air injection first and second holes extend through the forward and aft walls respectively. The segment may include first and second expansion joint features at distal first and second ends respectively of the segment. The segment may include a forward subcomponent including the cavity forward wall attached to an aft subcomponent including the cavity aft wall. The forward and aft subcomponents include forward and aft portions of the cavity radially outer wall respectively. A ring of the segments may be circumferentially disposed about an axis to form an annular segmented vortex cavity assembly.
Document ID
20100040615
Acquisition Source
Glenn Research Center
Document Type
Other - Patent
Authors
Grammel, Jr., Leonard Paul
Pennekamp, David Lance
Winslow, Jr., Ralph Henry
Date Acquired
August 24, 2013
Publication Date
August 24, 2010
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: US-Patent-7,779,866
Patent Application Number: US-Patent-Appl-SN-11/490,559
Funding Number(s)
CONTRACT_GRANT: NAS3-01135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,779,866
Patent Application
US-Patent-Appl-SN-11/490,559
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