Method for manufacturing a reinforced shell for forming...

Plastic and nonmetallic article shaping or treating: processes – Direct application of fluid pressure differential to... – Producing multilayer work or article

Reexamination Certificate

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Details

C156S285000, C156S286000, C156S242000, C156S245000, C244S119000

Reexamination Certificate

active

07897095

ABSTRACT:
The invention concerns a method for manufacturing a shell, in particular a fuselage shell, a wing shell, a horizontal stabilizer shell or a vertical stabilizer shell, that is reinforced with a plurality of stiffening elements, for forming component parts for aircraft with high dimensional stability, wherein the stiffening elements and a shell skin are made with epoxy resin from at least partially cured carbon fiber reinforced semi-finished parts, the method comprising the following steps:positioning the stiffening elements on the shell skin,abutting connecting elements against the shell skin and the stiffening elements, andcuring the connecting elements to form the shell.The invention also concerns a shell, in particular a fuselage shell, a wing shell, a horizontal stabilizer shell or a vertical stabilizer shell, manufactured in accordance with the inventive method.

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