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The Development of a Conical Composite Energy Absorber for Use in the Attenuation of Crash/Impact LoadsA design for a novel light-weight conical shaped energy absorbing (EA) composite subfloor structure is proposed. This composite EA is fabricated using repeated alternating patterns of a conical geometry to form long beam structures which can be implemented as aircraft subfloor keel beams or frame sections. The geometrical features of this conical design, along with the hybrid composite materials used in the manufacturing process give a strength tailored to achieve a constant 25-40 g sustained crush load, small peak crush loads and long stroke limits. This report will discuss the geometrical design and fabrication methods, along with results from static and dynamic crush testing of 12-in. long subcomponents.


Document ID
20150001245
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Littell, Justin D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
February 3, 2015
Publication Date
September 8, 2014
Subject Category
Composite Materials
Structural Mechanics
Aircraft Design, Testing And Performance
Report/Patent Number
NF1676L-18267
Report Number: NF1676L-18267
Meeting Information
Meeting: ASTM-D30 Committee Meeting
Location: La Jolla, CA
Country: United States
Start Date: September 8, 2014
End Date: September 11, 2014
Sponsors: Japan Society for Composite Materials, ASTM International, American Society for Composites
Funding Number(s)
WBS: WBS 380046.02.07.04.01.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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