NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Method for stabilizing thick honeycomb core composite articlesA method of stabilizing thick honeycomb core composites is disclosed. The method comprises bonding a layer of resin impregnated woven graphite fibers to one surface of the honeycomb core, then curing the resin impregnates forming a stabilized honeycomb core. This stabilized core is then cut to net shape and the composite structure is formed by laying one or more resin impregnated fiber layers onto the stabilized core surf aces and curing the lay-up under heat and pressure forming the composite article. Also disclosed is a stabilized honeycomb subassembly formed by bonding a graphite fiber, resin impregnated layer onto one of the honeycomb core surfaces and curing the resins, then shaping the stabilized honeycomb core to the desired form.
Document ID
19910021910
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Gary J Jacaruso
(United Technologies Corporation (United States) Windsor Locks, Connecticut, United States)
Date Acquired
August 14, 2013
Publication Date
July 14, 1987
Publication Information
Publisher: United States Patent and Trademark Office
Subject Category
Composite Materials
Report/Patent Number
Patent Number: INT-PATENT-1-253-424
Accession Number
91N31224
Funding Number(s)
CONTRACT_GRANT: N00019-82-C-0127
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
4,680,216 | CA 1253424
Patent Application
647,308 | CA 518103
No Preview Available