Fiber resin composites, and method of making the same

Details Fiber resin composites, and method of making the same Fiber resin composites, and method of making the same

B - Operations, Transporting

32

B

204/91.41

B32B 1/08 (2006.01) B29C 35/02 (2006.01) B29C 35/08 (2006.01) B29C 35/18 (2006.01) B29C 53/84 (2006.01) B29C 70/52 (2006.01) B32B 5/22 (2006.01) B65H 81/00 (2006.01) C08J 3/24 (2006.01) B29C 53/56 (2006.01)

Patent

CA 1335494

A fiber/resin composite (40) whose resin phase is formed by at least initial actinic radiation curing of a resin composition comprising an actinic radiation curable first resin component and a second resin component which is non-cured under curing conditions effective for the first resin component. The actinic radiation exposure of the fiber/resin composition effects curing of the first resin component to immobilize the composite and impart structural integrity thereto, whereby the composite may be handled, packaged, or further processed. Filament wound, braided, and pultruded articles are described, together with associated methods for forming such articles by filament winding, braiding and pultrusion. As a specific embodiment, a solid fuel rocket motor (80) is disclosed comprising a solid fuel body (64) in a filament wound fiber-resin composite casing (82) formed by filament winding of the solid fuel body with resin-impregnated filament or rovings (76) thereof.

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