Forming a composite structure by filament placement on a tool surface of a tablet
First Claim
1. A method for forming a composite structure, using an automated placement head for placing pre-impregnated fiber or pre-impregnated tape onto a tool surface, the method comprising:
- providing a tooling tablet having a first and second substantially oppositely facing surface thereof, joined around the peripheries thereof by a side surface of the tablet, with at least one of the first and second surfaces forming a tool surface of the tablet;
mounting the tooling tablet adjacent the placement head, with the tool surface oriented substantially vertical and facing the placement head; and
placing a first set of pre-impregnated fibers and/or pre-impregnated tape onto a tool surface with the placement head to form the composite structure.
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Accused Products
Abstract
A method and apparatus are provided for forming a composite structure with an automatic placement head, through the use of a non-rotating tooling tablet having first and second substantially oppositely facing surfaces thereof, joined around the peripheries thereof by a side surface of the tablet, with at least one of the first or second surfaces forming a tool surface of the tablet. Layers of pre-impregnated fiber or tape are applied to the tool surface of the tablet by the automated fiber placement head.
62 Citations
21 Claims
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1. A method for forming a composite structure, using an automated placement head for placing pre-impregnated fiber or pre-impregnated tape onto a tool surface, the method comprising:
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providing a tooling tablet having a first and second substantially oppositely facing surface thereof, joined around the peripheries thereof by a side surface of the tablet, with at least one of the first and second surfaces forming a tool surface of the tablet;
mounting the tooling tablet adjacent the placement head, with the tool surface oriented substantially vertical and facing the placement head; and
placing a first set of pre-impregnated fibers and/or pre-impregnated tape onto a tool surface with the placement head to form the composite structure. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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- 12. An apparatus for forming a composite structure, the apparatus comprising a tooling tablet having a first and second substantially oppositely facing surface thereof, joined around the peripheries thereof by a side surface of the tablet, with at least one of the first and second surfaces forming one or more tool surfaces of the tablet, the tool surface being adapted for receiving pre-impregnated fiber and/or pre-impregnated tape from an automated placement head.
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21. An apparatus for forming an upper and a lower aircraft wing skin, the apparatus comprising, a tooling tablet having first and second substantially oppositely facing surfaces thereof, joined around the peripheries thereof by a side surface of the tablet, with the first surface defining a first tool surface for forming the upper wing skin and the second surface defining a second tool surface for forming the lower wing skin separate from the upper wing skin, the first and second tool surfaces being adapted for separately receiving pre-impregnated fiber and/or pre-impregnated tape from one or more automated placement heads operatively disposed adjacent one or both of the first and second surfaces of the tablet.
Specification