Wrinkle control method and tool therefor
AssigneeAirbus Operations GmbH
InventorsStephen Williams, Timothy Sanderson
Life of this patent
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AssigneeAirbus Operations GmbH
InventorsStephen Williams, Timothy Sanderson
Estimating the term…
A method for forming a laminate component, the method comprising the steps of: a) providing a tool having a molding surface; b) arranging a stack of ply layers on the molding surface of the tool; and c) molding the stack of ply layers over the molding surface in a molding process, wherein the tool has a wrinkle control feature in its molding surface for managing the development of wrinkle in the ply layers during the molding process, and wherein the wrinkle control feature cooperates with the stack of ply layers during the molding process to produce a local surface undulation in a nominal surface of the laminate component nearest the tool to either prevent wrinkling in the ply layers or initiate wrinkling in one or more of the ply layers at a predetermined location. Also, a tool having a wrinkle control feature, and a laminate component so formed.
A method for forming a composite spar comprising:
Dependencies are inferred from the claim text.