Konturformung in einem Faserplatziersystem
Anmelder: The Boeing Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4023421
- Aktenzeichen
- EP21216083
- Anmeldetag
- 20. Dezember 2021
- Veröffentlichung
- 9. Oktober 2024
- Erteilung
- 9. Oktober 2024
- Rechtsraum
- EP
- IPC
- B29C70/38B29C70/54B29C70/34
Abstract
A method for contour forming in a fiber placement system. The method includes painting (304) a plurality of sliced layers on a stationary form to create a composite component, wherein the plurality of sliced layers includes a plurality of hoop tows, and one or more overlap splices are formed in each of the plurality of hoop tows; applying (306) a layup heat to a plurality of target areas on the plurality of sliced layers during the painting, wherein the plurality of target areas is spatially arranged to permit a slippage in the plurality of overlap splices; draping (312) the composite component on a curved tool with the plurality of hoop tows oriented perpendicular to an axis of curvature of the curved tool; and applying (320) a curing heat to the composite component after the composite component has been contoured by the curved tool, wherein the curing heat inhibits a further slippage in the plurality of overlap splices.
Anmelder
- Firma
- The Boeing Company
- Land
- 🇺🇸 USA
US-amerikanischer Luft- und Raumfahrtkonzern mit Sitz in Virginia. Entwickelt und fertigt Verkehrsflugzeuge, Militärflugzeuge, Raumfahrtsysteme sowie Verteidigungs- und Sicherheitstechnik.
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