Fabrication of large hollow composite structure with precisely d

Details Fabrication of large hollow composite structure with precisely d Fabrication of large hollow composite structure with precisely d

1995-05-10

1997-11-04

Timm, Catherine

Plastic and nonmetallic article shaping or treating: processes

Direct application of fluid pressure differential to...

Producing multilayer work or article

264225, 264313, 264510, 425175, 425388, 425390, B29C 7028

Patent

active

056836465

ABSTRACT:
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.

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