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Integrated gas turbine engine-nacelleA nacelle for use with a gas turbine engine is presented. An integral webbed structure resembling a spoked wheel for rigidly interconnecting the nacelle and engine, provides lightweight support. The inner surface of the nacelle defines the outer limits of the engine motive fluid flow annulus while the outer surface of the nacelle defines a streamlined envelope for the engine.
Document ID
19780010123
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Adamson, A. P. (NASA Lewis Research Center Cleveland, OH, United States)
Sargisson, D. F. (NASA Lewis Research Center Cleveland, OH, United States)
Stotler, C. L., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 25, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: NASA-CASE-LEW-12389-2
Patent Number: US-PATENT-4,055,041
Patent Application Number: US-PATENT-APPL-SN-628221
Accession Number
78N18066
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-12389-2|US-PATENT-4,055,041
Patent Application
US-PATENT-APPL-SN-628221

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