NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Metal matrix composite structural panel constructionLightweight capped honeycomb stiffeners for use in fabricating metal or metal/matrix exterior structural panels on aerospace type vehicles and the process for fabricating same are disclosed. The stiffener stringers are formed in sheets, cut to the desired width and length and brazed in spaced relationship to a skin with the honeycomb material serving directly as the required lightweight stiffeners and not requiring separate metal encasement for the exposed honeycomb cells.
Document ID
19840003146
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Mcwithey, R. R.
(NASA Langley Research Center Hampton, VA, United States)
Royster, D. M.
(NASA Langley Research Center Hampton, VA, United States)
Bales, T. T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
October 25, 1983
Subject Category
Composite Materials
Report/Patent Number
Patent Number: NASA-CASE-LAR-12807-1
Patent Application Number: US-PATENT-APPL-SN-280155
Patent Number: US-PATENT-4,411,380
Accession Number
84N11214
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LAR-12807-1|US-PATENT-4,411,380
Patent Application
US-PATENT-APPL-SN-280155
No Preview Available