Epoxy resin system and pultrusion process employing same
AssigneeLockheed Corporation
InventorTed H. Thorsted, Jr.
Life of this patent
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AssigneeLockheed Corporation
InventorTed H. Thorsted, Jr.
Estimating the term…
An epoxy resin system is disclosed which is especially adapted for use in the pultrusion process. Such resin system comprises tris (hydroxyphenyl) methane-based epoxy resin and a combination of the cross-linking agents (methyl)-bicyclo(2,2,1) heptane-2,3-dicarboxylic anhydride and poly sebacic poly anhydride, the ratio of the dicarboxylic anhydride to the total amount of cross-linking agents ranging from 0.65 to 0.80 and the ratio of the poly anhydride to the total amount of cross-linking agents ranging from 0.35 to 0.20. The amount of total cross-linking agents to epoxy resin ranges from about 60 to about 80 parts total cross-linking agents, per 100 parts resin, by weight. A small amount of an imidazole accelerator, preferably 2-ethyl-4 methyl imidazole, is included. The pultrusion process includes the steps of creeling a plurality of fabric bands or individual fiber tows, collating the creeled bands, passing the array of collated bands through the above epoxy resin system heated in a wet-out tank, passing the wetted array of fabric bands through a forming guide to form a resin impregnated laminate, passing the laminate through a heated pultrusion die, and discharging a continuous length of cured fiber-epoxy composite from the die.
A pultrusion process for the production of fiber-resin composite which comprises:
A pultrusion process for the production of fiber-resin composite which comprises:
Dependencies are inferred from the claim text.