| 摘要 |
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.
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