Aircraft structure including composite beam and composite...

Details Aircraft structure including composite beam and composite... Aircraft structure including composite beam and composite...

2011-01-25

2011-01-25

Dinh, Tien (Department: 3644)

Aeronautics and astronautics

Aircraft structure

Details

Reexamination Certificate

active

07874518

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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