Splice joint in laminate composite structure
AssigneeTextron Innovations Inc.
InventorSebastien Duval
Life of this patent
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AssigneeTextron Innovations Inc.
InventorSebastien Duval
Estimating the term…
Layers of plies of composite material are laid on a convex tool surface. A first layer is placed with a first ply of a first section having a gap edge adjacent a gap edge of a first ply of a second section, the edges being parallel and a contraction distance from each other. A second layer is placed with a second ply of the first section having a gap edge adjacent a gap edge of a second ply of the second section, the edges being parallel and a contraction distance from each other, the second ply of the second section overlapping onto the first ply of the first section by a splice distance. Consolidation and curing cause contraction of the layers toward the tool, allowing the adjacent gap edges of each layer to be in close proximity or in contact after moving toward each other during the contraction.
A method for forming a composite structure of first and second sections joined by a splice joint, each section being formed from uncured layers of plies of composite material, each ply being formed from fibers and a volume of uncured matrix material and having a gap edge, the method comprising:
A method for forming a closed-shape composite structure of first and second sections joined by a splice joint, each section being formed from uncured layers of plies of composite material, each ply being formed from fibers and a volume of uncured matrix material and having a gap edge, the method comprising:
Dependencies are inferred from the claim text.