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Novel cost controlled materials and processing for primary structuresTextile laminates, developed a number of years ago, have recently been shown to be applicable to primary aircraft structures for both small and large components. Such structures have the potential to reduce acquisition costs but require advanced automated processing to keep costs controlled while verifying product reliability and assuring structural integrity, durability and affordable life-cycle costs. Recently, resin systems and graphite-reinforced woven shapes have been developed that have the potential for improved RTM processes for aircraft structures. Ciba-Geigy, Brochier Division has registered an RTM prepreg reinforcement called 'Injectex' that has shown effectivity for aircraft components. Other novel approaches discussed are thermotropic resins producing components by injection molding and ceramic polymers for long-duration hot structures. The potential of such materials and processing will be reviewed along with initial information/data available to date.
Document ID
19950022409
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dastin, S. J.
(Grumman Aircraft Engineering Corp. Bethpage, NY, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Publication Information
Publication: NASA. Langley Research Center, Third NASA Advanced Composites Technology Conference, Volume 1, Part 2
Subject Category
Composite Materials
Accession Number
95N28830
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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