Verfahren zum automatisierten, klebtechnischen Fügen großflächiger Komponenten im Luftfahrzeugbau

The invention relates to a method for adhesively joining at least two large joining partners in vehicle construction, in particular in aircraft construction. Said method consists of the following steps: the geometric data of the joining partners is automatically determined; the joining gap measurements of the joining partners is determined from the geometric data; adhesive is applied to one or more joining surfaces of two joining partners which are to be joined in accordance with the joining gap measurements; the joining partners are joined in the joining position and joining pressure is sequentially applied to the joining surfaces along the joining gap for placing the joining partners into the final joining position.