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In Situ Composite FastenerFasteners installed prior to curing. In situ composite fastener polymeric, graphite, glass, or metallic thread, pin, or staple. Selected fastener pressed through thickness of composite component while composite is in prepreg or B-stage state. Parts not removed from mold to install fastener. Technique used around cutouts to prevent free edges from delaminating.
Document ID
19830000463
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Freeman, W. T., Jr. (U.S. Army Aviation Research and Development Command)
Jones, W. S.
Farley, G. L.
Date Acquired
August 11, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 1
ISSN: 0145-319X
Subject Category
Fabrication Technology
Report/Patent Number
LAR-12939
ISSN: 0145-319X
Report Number: LAR-12939
Accession Number
83B10463
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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