Method for manufacturing an aeronautical torsion box, torsion box and tool for manufacturing an aeronautical torsion box
US-2015343702-A1 · Dec 3, 2015 · US
US8945455B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8945455-B2 |
| Application number | US-201113288393-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 3, 2011 |
| Priority date | Nov 11, 2010 |
| Publication date | Feb 3, 2015 |
| Grant date | Feb 3, 2015 |
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A support apparatus and method for providing structural support to a shape memory polymer (SMP) apparatus during fabrication of composite parts. The support apparatus may comprise an adjustable, rigid structural member and a plurality of SMP support components transitionable between a rigid and malleable state and fixed to an outer surface of the rigid structural member. The rigid structural member may extend in at least one cross-sectional dimension toward the SMP apparatus, pressing the SMP support components, in their malleable state, against the SMP apparatus. The SMP support components may thereby conform to a first surface of the SMP apparatus, then return to their rigid state while pressed against the SMP apparatus, thus providing a rigid load path between the SMP apparatus and the rigid structural member. Then composite material may be applied to a second surface of the SMP apparatus, opposite of the first surface.
Opening claim text (preview).
Having thus described various embodiments of the invention, what is claimed as new and desired to be protected by Letters Patent includes the following: 1. A support apparatus configured for providing structural support to any apparatus, mold, tooling, or shape memory polymer (SMP) apparatus for forming composite parts, the support apparatus comprising: an adjustable, rigid structural member having adjustable cross-sectional dimensions, wherein the rigid structural member comprise…
Operations & Transport · mapped topic
Operations & Transport · mapped topic
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