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Method of insetting predesigned disbond areas into composite laminatesThis invention is a process for producing composite laminates containing interlaminar disbonds of controlled sizes, shapes, and positions within a composite structure. A composite layer is provided for later inclusion within a laminate. The surfaces of this composite layer are solvent cleaned and sandblasted, except in desired disbond areas, which are coated with a releasing surface. A template to mask the bond areas is employed to obtain disbond areas of controlled shapes and sizes. The resulting composite layer is then used in the subsequent manufacture of a laminate, whereby faulty adhesion in the laminate can be studied with prior knowledge of the size, shape, and location of the disbond areas.
Document ID
19900015881
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Dickerson, George E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
May 8, 1990
Subject Category
Composite Materials
Report/Patent Number
Patent Number: US-PATENT-4,923,545
Patent Number: NASA-CASE-LAR-13225-1
Patent Application Number: US-PATENT-APPL-SN-248018
Accession Number
90N25197
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,923,545|NASA-CASE-LAR-13225-1
Patent Application
US-PATENT-APPL-SN-248018
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