Patent ID: 8540286

Claim:
A moulding core assembly, comprising: a moulding core for producing a fibre composite component for aerospace; a base element comprising a receiving portion for receiving the moulding core via a coupling portion of the moulding core and for subjecting the moulding core to a medium; a clamping element for fixing and sealing the coupling portion of the moulding core to the base element; at least one sealing element arranged between the base element and the clamping element for sealing the coupling portion of the moulding core to the base element; and a locking mechanism for locking the clamping element and the coupling portion of the moulding core, wherein the locking mechanism has a clamping device with a clip and a lever; and wherein the sealing element can be compressed in a sealing manner on the surface of the coupling portion of the moulding core and on the surface of the receiving portion of the base element.