Filamentary structural module for composites

Details Filamentary structural module for composites Filamentary structural module for composites

B - Operations, Transporting

32

B

154/70

B32B 5/08 (2006.01) B32B 15/02 (2006.01) C22C 47/20 (2006.01)

Patent

CA 1259018

Abstract of the Disclosure This invention includes a continuous in-plane spiral of monofilament/metallic ribbon which forms a preform for metal matrix composite fabrication. The purpose is to provide continuous spiral filament reinforcement around a hole or central core. This spiral monolayer is fabricated by co-winding the fila- ment and a ribbon or wire made from the intended composite material around a mandrel. Monolayers so constructed could then be stacked to form cylindrical or torus-shaped components and consolidated in a direction parallel to the axis of the shape.

496873

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