| タイトル | PRSEUS Panel Fabrication Final Report |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140006175 |
| 著者（英） | Linton, Kim A.; Turley, Robert; Hoffman, Krishna; Pickell, Robert; Velicki, Alexander; Thrash, Patrick |
| 発行日 | 2014-01-01 |
| 言語 | eng |
| 内容記述 | NASA 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. |
| NASA分類 | Aircraft Design, Testing and Performance; Structural Mechanics |
| レポートNO | NF1676L-18009
NASA/CR-2014-218149 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
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