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Composite aircraft structure having lightning protectionA lightning protection system for advanced composite aircraft structures consisting of a sandwich structure including two layers of aluminum foil separated by a layer of dielectric material. The sandwich structure is applied to the surface of the composite aircraft structure desired to be protected from lightning strike damage thereby confining damage to the sandwich structure which can be removed and replaced.
Document ID
20080004217
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Olson, Glenn O.
Date Acquired
August 24, 2013
Publication Date
September 28, 1982
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-254799
Patent Number: US-PATENT-4,352,142
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,352,142
Patent Application
US-PATENT-APPL-SN-254799

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