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Application of advanced material systems to composite frame elementsA three phase program has been conducted to investigate DuPont's Long Discontinuous Fiber (LDF) composites. Additional tests were conducted to compare LDF composites against toughened thermosets and a baseline thermoset system. Results have shown that the LDF AS4/PEKK offers improved interlaminar (flange bending) strength with little reduction in mechanical properties due to the discontinuous nature of the fibers. In the third phase, a series of AS4/PEKK LDF C-section curved frames (representing a typical rotorcraft light frame) were designed, manufactured and tested. Specimen reconsolidation after 'stretch forming' and frame thickness were found to be key factors in this light frame's performance. A finite element model was constructed to correlate frame test results with expected strain levels determined from material property tests. Adequately reconsolidated frames performed well and failed at strain levels at or above baseline thermoset material test strains. Finally a cost study was conducted which has shown that the use of LDF for this frame would result in a significant cost savings, for moderate to large lot sizes compared with the hand lay-up of a thermoset frame.
Document ID
19950022011
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Llorente, Steven
(Boeing Defense and Space Group Philadelphia, PA, United States)
Minguet, Pierre
(Boeing Defense and Space Group Philadelphia, PA, United States)
Fay, Russell
(Boeing Defense and Space Group Philadelphia, PA, United States)
Medwin, Steven
(Du Pont de Nemours, E. I. and Co., Wilmington DE., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Publication Information
Publication: FAA, Ninth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Volume 1
Subject Category
Composite Materials
Accession Number
95N28432
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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