Method for fabricating reinforced composite materials

Coating processes – With post-treatment of coating or coating material – Vacuum or reduced pressure utilized

Reexamination Certificate

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C156S174000, C156S285000, C156S312000, C156S307100, C164S098000, C264S102000, C264S257000, C264S258000, C264S510000, C427S288000, C427S384000, C427S394000, C428S293400, C428S295100, C428S297400, C428S298700

Reexamination Certificate

active

07867566

ABSTRACT:
A method for fabricating a reinforced matrix composite comprising the step of providing a composite preform having a fibrous structure and applying matrix material onto the preform in locations along the preform. A barrier material is applied to at least a portion of the coated preform to direct the flow of matrix material into the preform. The composite preform is heated to a temperature sufficient to render the matrix material viscous and insufficient to cure the matrix material. The pressure to the interior of the composite preform is reduced, while the pressure to the barrier material is increased. The temperature is maintained to flow the matrix material into the composite preform and to force gases from the fibrous structure. The composite preform is then cured and cooled to form a reinforced matrix composite having a low void content and a substantially uniform matrix distribution.

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