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Integrated gas turbine engine-nacelleA nacelle for use with a gas turbine engine is provided with an integral webbed structure resembling a spoked wheel for rigidly interconnecting the nacelle and engine. The nacelle is entirely supported in its spacial relationship with the engine by means of the webbed structure. 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
19790005925
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Adamson, A. P. (GE Cincinnati, United States)
Sargisson, D. F. (GE Cincinnati, United States)
Stotler, C. L., Jr. (GE Cincinnati, United States)
Date Acquired
September 3, 2013
Publication Date
January 2, 1979
Subject Category
Aircraft Propulsion And Power
Accession Number
79N14096
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,132,069|NASA-CASE-LEW-12389-3
Patent Application
US-PATENT-APPL-SN-552108|US-PATENT-APPL-SN-753452

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