Shape-distorting tooling system and method for curing composite parts
AssigneeThe Boeing Company
InventorsRobert T. Loftus, Jr., Jason M. Robinson, Mitchell J. Lee
Life of this patent
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AssigneeThe Boeing Company
InventorsRobert T. Loftus, Jr., Jason M. Robinson, Mitchell J. Lee
Estimating the term…
A tooling system may include a cure tool and a biasing element. The cure tool may have a cure tool coefficient of thermal expansion (CTE) and may be configured for curing a composite article formed of two or more components having dissimilar component CTEs. The biasing element may be fixedly attached to the cure tool and has a biasing element CTE that may be different than the cure tool CTE. The biasing element may be configured such that a combination of the cure tool CTE and the biasing element CTE causes a heat-up displacement in the cure tool when heated and the composite article is cured in a distorted shape. When the cured composite article is cooled, the cured composite article may substantially assume an as-designed shape.
A method of manufacturing a composite article, comprising:
Dependencies are inferred from the claim text.