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PRSEUS Panel Fabrication Final ReportNASA and the Boeing Company have been working together under the Environmentally Responsible Aviation Project to develop stitched unitized structure for reduced weight, reduced fuel burn and reduced pollutants in the next generation of commercial aircraft. The structural concept being evaluated is PRSEUS (Pultruded Rod Stitched Efficient Unitized Structure). In the PRSEUS concept, dry carbon fabric, pultruded carbon rods, and foam are stitched together into large preforms. Then these preforms are infused with an epoxy resin into large panels in an out-of-autoclave process. These panels have stiffeners in the length-wise and width-wise directions but contain no fasteners because all stiffeners are stitched to the panel skin. This document contains a description of the fabrication of panels for use in the 30-foot-long Multi-Bay Box test article to be evaluated at NASA LaRC.
Document ID
20140006175
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Linton, Kim A.
(Boeing Co. Huntington Beach, CA, United States)
Velicki, Alexander
(Boeing Co. Huntington Beach, CA, United States)
Hoffman, Krishna
(Boeing Co. Huntington Beach, CA, United States)
Thrash, Patrick
(Boeing Co. Huntington Beach, CA, United States)
Pickell, Robert
(Boeing Co. Huntington Beach, CA, United States)
Turley, Robert
(Boeing Co. Huntington Beach, CA, United States)
Date Acquired
May 23, 2014
Publication Date
January 1, 2014
Subject Category
Aircraft Design, Testing And Performance
Structural Mechanics
Report/Patent Number
NASA/CR-2014-218149
NF1676L-18009
Report Number: NASA/CR-2014-218149
Report Number: NF1676L-18009
Funding Number(s)
CONTRACT_GRANT: NNL13AA11C
WBS: WBS 699959.02.22.07.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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