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Multi-Fiber CompositesResin matrix composites having improved resistance to foreign object damage in gas turbine engine fan blade applications were developed. Materials evaluated include epoxy matrix graphite/glass and boron/glass hybrids, thermoplastic matrix boron/glass hybrids, and superhybrids consisting of graphite/epoxy, boron/aluminum, and titanium alloy sheets. Static, pendulum impact, and ballistic impact test results are reported for all materials. Superhybrid blade like specimens are shown to be capable of withstanding relatively severe ballistic impacts from gelatin spheres without fracture. The effects of ply configuration and projectile angle of incidence on impact behavior are described. Predictions of surface strains during ballistic impact are presented and shown to be in reasonable agreement with experimental measurements.
Document ID
19760024210
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Novak, R. C.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-135062
R76-912098-11
Report Number: NASA-CR-135062
Report Number: R76-912098-11
Accession Number
76N31298
Funding Number(s)
CONTRACT_GRANT: NAS3-18941
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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