B - Operations – Transporting – 29 – C
Patent
B - Operations, Transporting
29
C
B29C 70/44 (2006.01) B29D 99/00 (2010.01) B29C 33/38 (2006.01) B29C 33/50 (2006.01)
Patent
CA 2652096
The invention relates to a method and a moulding core for producing a fibre composite component (34), in particular in aerospace, comprising the following method steps: introducing a core sleeve (9) into a moulding tool (2) for establishing an outer geometry of a moulding core (27) to be formed; filling the core sleeve (9) that is introduced with a vacuum-fixable filling material (21); applying a vacuum to the core sleeve (9) and consequently vacuum-fixing the filling material (21) for forming the moulding core (27); and at least partly laying at least one semifinished fibre product (33a, 33b) on the moulding core (27) that is formed, for the shaping of the fibre composite component (34) to be produced.
L'invention concerne un procédé et un noyau de moulage destinés à la production d'un élément composite à fibres (34), en particulier pour l'aérospatiale. Le procédé consiste: à introduire un manchon noyau (9) dans un outil de moulage (2) afin d'établir la géométrie externe d'un noyau de moulage (27) à former; à remplir le manchon noyau (9) qui est introduit avec un matériau de remplissage (21) pouvant être fixé par le vide; à appliquer le vide au manchon noyau (9) et à fixer par la suite le matériau de remplissage (21) afin de former le noyau de moulage (27); et à disposer au moins partiellement au moins un produit à fibres semi-fini (33a, 33b) sur le noyau de moulage (27) formé afin de donner une forme à l'élément composite à fibres (34) à produire.
Jacob Torben
Piepenbrock Joachim
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Sim & Mcburney
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