Process for the production of a component, and fibre-reinforced thermoplastic component
AssigneeAirbus Operations GmbH
InventorsKlaus Edelmann, Tanja Frese, Timo Stoeven, Tobias Wirtz
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AssigneeAirbus Operations GmbH
InventorsKlaus Edelmann, Tanja Frese, Timo Stoeven, Tobias Wirtz
Estimating the term…
The invention relates to a method for producing a component for connecting a fuselage cell skin to an annular rib of an aircraft, wherein the component is formed by bending of a flat blank along at last two edge lines and wherein the blank is formed by a CFRP. According to the invention the interlaminar sliding of the fiber layers is largely completed in a first forming step, while in a second forming step a consolidation of the component takes place by the use of pressure from the press on all sides by means of an upper tool and a lower tool. This enables complex components with at least two edge lines to be produced, which edge lines run at angles of approximately, preferably at angles of 309° to 90°, to each other, and which edge lines also lie in at least two different planes.
A method of producing a component with the following steps:
Dependencies are inferred from the claim text.