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Aircraft engine nozzleA variable area exit nozzle arrangement for an aircraft engine was a substantially reduced length and weight which comprises a number of longitudinally movable radial vanes and a number of fixed radial vanes. The movable radial vanes are alternately disposed with respect to the fixed radial vanes. A means is provided for displacing the movable vanes along the longitudinal axis of the engine relative to the fixed radial vanes which extend across the main exhaust flow of the engine.
Document ID
19800023884
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Sorensen, N. E.
(NASA Ames Research Center Moffett Field, CA, United States)
Latham, E. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
July 29, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-023436
Patent Number: US-PATENT-4,214,703
Patent Number: NASA-CASE-ARC-10977-1
Accession Number
80N32392
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,214,703|NASA-CASE-ARC-10977-1
Patent Application
US-PATENT-APPL-SN-023436
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