Method to create bends in composite panels

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United States of America Patent

PATENT NO 8234901
APP PUB NO 20090107312A1
SERIAL NO

11924125

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A method for forming a bend in composite panel. In one advantageous embodiment, a method is used to form a bend in a composite panel. An angle and a radius bend are identified for the bend. A location of the bend in the composite panel is identified. A slot is cut having a curved flange in the composite panel at the identified location in a single pass through the composite panel with a tool, wherein the curved flange has a shape with a bend allowance width and a bend slot width. The bend allowance width is BA=2π*A/360, wherein BA is the bend allowance width, R is a corner radius, and A is a bend angle. The bend slot width is BS=BA−2K(R−T), wherein K is Tan(A/2) and T is a thickness of the composite panel. The composite panel with the slot is bent to form the bend.

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Patent Owner(s)

  • THE BOEING COMPANY

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Lewis, Michael Steven Lake Forest Park, US 8 47
Roets, Guy Wade Duvall, US 2 18

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