Method to eliminate undulations in a composite panel

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

Reexamination Certificate

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Details

C156S307700, C244S131000, C264S102000

Reexamination Certificate

active

07052573

ABSTRACT:
A method and article of manufacture of joining a stringer to a wing or tail panel and curing a wing or tail panel is disclosed. A sheet of titanium is placed between a cured stringer and an uncured wing or tail panel. The stringer, wing or tail panel and sheet are then placed within a vacuum bag, and gas is pumped out of the bag. The bag is then placed in an auto-clave to cure the wing or tail panel.

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patent: 1 134 070 (2001-09-01), None
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English abstract for JP 11207868.
International Search Report mailed Dec. 16, 2005.

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