| 摘要 |
The invention is directed to a method for producing a Fiber Metal Laminate component of an airplane, using a manipulator system (1) with an end effector (3) and a control (4) assigned to the manipulator system (2), wherein at least one metal layer (5) and at least one unhardened fiber layer (6) are being stacked onto each other in a mould (7) by the manipulator system (2) in a stacking sequence, wherein each stacking cycle comprises picking up a metal layer (5) or a fiber layer (6) from a respective supply stack (8, 9) according to the stacking sequence, transporting the layer (5, 6) to the mould (7), placement of the layer (5, 6) at a deposition surface in the mould (7) according to the stacking sequence and depositing the so placed layer (5, 6) onto the deposition surface (10). It is proposed that after being picked up from the supply stack (8, 9) and before being deposited onto the deposition surface (10) the layer (5, 6) to be stacked is being deformed by the end effector (3) as to adapt the form of the layer (5, 6) to the form of the deposition surface (10). |
