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US 10,793,250 B2Granted
Apparatus configured as a structure comprising a skin including a bond without a splice plate
AssigneeThe Boeing Company
InventorsGary Ernest Georgeson, Kenneth Harlan Griess
Life of this patent
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Abstract
A composite structure comprises stacked sets of laminated fiber reinforced resin plies and metal sheets. Edges of the resin plies and metal sheets are interleaved to form a composite-to-metal joint connecting the resin plies with the metal sheets.
Claims22
An apparatus configured as a structure comprising a skin, the skin comprising:
- a stack comprising metal sheets;
- a first section comprising a first composite laminate, the first composite laminate connected to a top side of a frame of the structure, and bonded to a first end of the stack to form a first composite-to-metal joint, wherein the metal sheets and the first composite laminate are non-interleaving except in the first composite-to-metal joint;
- and
- a second section comprising a second composite laminate, the second composite laminate connected to a bottom side of the frame, and bonded to a second end of the stack to form a second composite-to-metal joint, wherein the metal sheets and the second composite laminate are non-interleaving except in the second composite-to-metal joint.
1 more element
An apparatus configured as a structure comprising a skin, the skin comprising:
- a stack comprising metal sheets;
- a first section comprising a first composite laminate, the first composite laminate connected to a top side of a frame of the structure, and bonded without a splice plate, to a first end of the stack;
- a second section comprising a second composite laminate, the second composite laminate connected to a bottom side of the frame, and bonded to a second end of the stack;
- and
- a composite-to-metal bond at each end of the stack configured as a finger lap joint, wherein each finger lap joint comprises four plies of composite laminate abutting each metal sheet in the stack, each metal sheet in the stack being:
- about 0.025 inches thick, and bonded to an adjacent metal sheet by a layer of adhesive, wherein the metal sheets and the first composite laminate are non-interleaving except in a first composite-to-metal joint at the first end of the stack, and wherein the metal sheets and the second composite laminate are non-interleaving except in a second composite-to-metal joint at the second end of the stack,
- wherein the first section, the stack, and the second section, form a monolithic shell for the structure,
- wherein the structure comprises a wing box, and the metal sheets form a leading edge of a wing comprising the wing box, the leading edge being able to withstand, without material failure, at least twice an impact force relative to an alternate leading edge comprising only a composite skin, and
- wherein the stack comprises a shape memory alloy that changes, in response to a trigger, a shape of an edge of the structure.
6 more elements
Dependencies are inferred from the claim text.