Composite with through the thickness reinforcement
AssigneeThe United States of America as represented by the Adminstrator of the National Aeronautics and Space Administration
InventorGary L. Farley
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Abstract
A laminated composite material with improved interlaminar strength and damage tolerance having short rods distributed evenly throughout the composite material perpendicular to the laminae. Each rod is shorter than the thickness of the finished laminate, but several times as long as the thickness of each lamina. The laminate is made by inserting short rods in layers of prepreg material, and then stacking and curing prepreg material with rods inserted therethrough.
Claims2
A laminated composite material having a predetermined thickness, comprising:
- a plurality of rods wherein the rods are of a diameter ranging from 1 micron to about 2 mm and have lengths shorter than the total thickness of the composite material but several times as long as the thickness of each lamina of the composite material, arranged substantially parallel to the thickness of the composite material and distributed substantially evenly throughout the volume of the composite material.
A composite material having a predetermined finished thickness, comprising:
- (a) a stack of reinforced laminae bonded together in a matrix;
- and
- (b) a plurality of rods, said rods having diameters ranging from about 1 micron to about 2 mm, having a length substantially less than said finished thickness, but several times as long as the thickness of each lamina, said rods being arranged substantially perpendicular to the laminae and distributed substantially evenly throughout the composite material.
Dependencies are inferred from the claim text.