Methods for Making Composite Parts from Stacked Partially Cured Sublaminate Units
AssigneeThe Boeing Company
InventorGeoffrey A. Butler
Life of this patent
Estimating the term…
Loading patent…
AssigneeThe Boeing Company
InventorGeoffrey A. Butler
Estimating the term…
A method of forming a composite article. One step involves applying adhesive on surfaces of a plurality of sublaminate units, each ply of each sublaminate unit comprising fibers impregnated with resin which has been initially cured to 30% to 50% of full cure. The initially cured sublaminate units are then arranged in a stack, which stack is pressed against a surface of a forming tool. While pressure is being applied, the stack is heated to an intermediate temperature above a glass transition temperature of the resin for a time interval sufficient to intermediately cure the resin to 50% to 70% of full cure to form a composite laminate having a contour defined by the surface of the forming tool. Then the resin is finally cured at a final temperature higher than the intermediate temperature.
A method of forming a composite article, comprising:
A composite precursor comprising:
A method of forming a composite article, comprising:
Dependencies are inferred from the claim text.