Premium Aerotec Gmbh

Tim Neitzel

Klaus Edelmann

Angelos Miaris

Tanja Frese

Helmut Krumpen

Andreas Leis

Arnoldt Quiring

Jens Bahnsen

Philip Hasemann

Juergen Krone

Jürgen Krone

A method for producing a thermoplastic fiber composite component, in particular for an aircraft or spacecraft, has the following method steps: material-removing processing of a first face of a first plate, wherein the first plate comprises a thermoplastic fiber composite material and a local reduction in thickness of the first plate is made by the material-removing processing of the first face; positioning a second plate relative to the first plate such that the first face of the first plate is brought into alignment with a third face of the second plate; and joining the first plate to the second plate to form a single component, wherein the surface of the first face of the first plate is integrally bonded to the surface of the third face of the second plate.

Method for producing a thermoplastic fiber composite component

A semi-finished product arrangement for producing a fiber composite component by molding a planar semi-finished fiber composite product in a molding tool is provided. The arrangement includes the semi-finished fiber composite product and multiple holding elements fixed in place thereon and each extending beyond the edge of the semi-finished fiber composite product. The holding elements are countersunk in recesses of the semi-finished fiber composite product, in order to avoid a projection in terms of height.

Process for producing a fiber composite component, as well as a semi finished assembly for producing a fiber composite component

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Bremen, Germany

Tim Neitzel