FABRICATION OF LARGE HOLLOW COMPOSITE STRUCTURE

A method for fabricating a composite structure such as an aircraft radome includes preparing seamless female support mold/caul plate tooling, and seamless male support mold/vacuum bag tooling. An uncured composite structure is collated on the external surface of the male support mold/vacuum bag tool...

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Bibliographic Details
Main Author REILING, HENRY, E., JR
Format Patent
LanguageEnglish
French
German
Published 02.06.1999
Edition6
Subjects
AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
PERFORMING OPERATIONS
SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR
SHAPING OR JOINING OF PLASTICS
TRANSPORTING
WORKING OF PLASTICS
WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Summary:A method for fabricating a composite structure such as an aircraft radome includes preparing seamless female support mold/caul plate tooling, and seamless male support mold/vacuum bag tooling. An uncured composite structure is collated on the external surface of the male support mold/vacuum bag tooling, and then transferred to the female support mold/caul plate tooling for curing. The female support mold/caul plate tooling defines the outer surface of the final composite structure, permitting the outer surface of be smooth and of an aerodynamic shape.
Bibliography:Application Number: EP19960915621