Integrated Wiring System for Composite Structures
US-2015342077-A1 · Nov 26, 2015 · US
US9309007B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9309007-B2 |
| Application number | US-201213483186-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 30, 2012 |
| Priority date | May 31, 2011 |
| Publication date | Apr 12, 2016 |
| Grant date | Apr 12, 2016 |
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Disclosed is a jig for the modelling of at least one section of an aircraft fuselage, with a framework structure and with a multiplicity of adapters for the connection of stiffening elements to the framework structure, which can be moved relative to the framework structure, and/or with a multiplicity of adapters for the modelling of profiles of stiffening elements, which can be moved relative to the framework structure.
Opening claim text (preview).
The invention claimed is: 1. A jig for modelling at least one section of an aircraft fuselage comprising: a framework structure including a multiplicity of framework elements extending in a transverse direction of the fuselage; wherein the framework structure includes longitudinal guideways for moving the framework elements in a longitudinal direction of the fuselage; wherein the framework elements are slidably mounted on the longitudinal guideways such that individual spacing…
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