Lightweight structural component made of metallic ply materials

Details Lightweight structural component made of metallic ply materials Lightweight structural component made of metallic ply materials

B - Operations, Transporting

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B

B32B 15/08 (2006.01) B32B 3/10 (2006.01) B32B 3/24 (2006.01) B32B 7/12 (2006.01) B32B 15/00 (2006.01) B32B 15/02 (2006.01) B64C 1/00 (2006.01) B64C 30/00 (2006.01) B64D 1/00 (2006.01) F16S 1/00 (2006.01)

Patent

CA 2438417

A lightweight, laminated structural component, such as a skin section for an aircraft fuselage, is constructed of at least two sheet metal plies that are adhesively bonded to each other. One ply is an uninterrupted ply. The other ply is a lattice with open fields surrounded by strip shaped lands which fortify load exposed areas of the lamination. The open fields of the lattice make mechanical or chemical pocketing operations unnecessary. By shaping and positioning the strip shaped lands including struts in accordance with load patterns to which an aircraft skin is exposed in use, the skin characteristics cam be tailored as required.

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