| 摘要 |
<p>A forming tool (2) with a predefined mould portion (3) is provided in a method for producing a reinforced fibre composite component (1) for aviation and aerospace. A forming/support element (4) is moulded by means of the mould portion (3) of the forming tool (2). A semi-finished fibre product (5) is then deposited at least in portions on the shaped forming/support element (4). The deposited semi-finished fibre product (5) is deformed by means of the forming/support element (4) to form at least one reinforcing portion (7, 8, 9). The forming/support element (4) is then removed from the forming tool (2) together with the reinforcing section (7, 8, 9) formed on this element, followed by defined positioning of the reinforcing section (7, 8, 9) thus formed with respect to an associated fibre composite component portion (12) by supporting with the forming/support element (4). The reinforcing portion (7, 8, 9) is cured to form the reinforced fibre composite component (1). A forming device is provided with a predefined mould portion (3) which holds a forming/support element (4) such that it can be removed.</p> |
