Composite structure reinforcement

Stock material or miscellaneous articles – Structurally defined web or sheet – Including sheet or component perpendicular to plane of web...

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156285, 156287, 4283179, 4283191, B32B 326, B32B 704

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048084611

ABSTRACT:
Translaminar reinforcement structure for localized Z-direction reinforcement of composite structure includes a body of thermally decomposable material that has substantially opposed surface, a plurality of reinforcing elements in the body that extend generally perpendicularly to one body surface, and pressure intensifying structure on the other opposed body surfaces for applying driving force to the reinforcing elements for insertion into the composite structure as the body is subjected to elevated temperature and decomposes.

REFERENCES:
patent: 4136226 (1979-01-01), Gilman
patent: 4177306 (1979-12-01), Schulz et al.
patent: 4274901 (1981-06-01), Elber
patent: 4361613 (1982-11-01), Bogner et al.
patent: 4469740 (1984-09-01), Bailly
patent: 4637947 (1987-01-01), Maekawa et al.
Kim, et al., "Initiation of Delamination of Composite Laminates", Proceedings of U.S.-Japan Joint Conference on Exp. Analysis, SESA, Hawaii, May, 1982, pp. 244-251.
Kim, et al., "Experimental and Analytical Studies on the Onset of Delamination in Laminated Composites", Journal of Composite Materials, vol. 18, Jan., 1984, pp. 70-80.
Sawyer, "Effect of Stitching on the Strength of Bonded Composite Single Lap Joints", AIAA Journal, vol. 23, No. 11, pp. 1744-1748.

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