Method of forming panels using an in-situ tape placement...

Adhesive bonding and miscellaneous chemical manufacture – Methods – Surface bonding and/or assembly therefor

Reexamination Certificate

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Details

C156S175000, C156S173000, C156S189000, C156S191000, C156S193000

Reexamination Certificate

active

08043458

ABSTRACT:
A composite panel and method of manufacture includes a support structure and a tape skin wound about the support structure. A mandrel assembly with extractable longitudinal mandrels facilitates winding of the tape skin onto the support structure. The composite panel is suitable for use in an aircraft floor system.

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International Search report and written opinion mailed Sep. 23, 2008.
X. Zhang, L. Hounslow, M. Grassi, “Improvement of Low-Velocity Impact and Compression-After-Impact Performance by Z-Fibre Pinning,” Composites Science and Technology, 66 92006); 2785-2794.
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