Within the framework of the DFG Collaborative Research Centre 401 "Flow Influence and Flow-Structure Interaction on Aerofoils", measurements of the vorticity wake of aerofoils are carried out at the Institute of Aeronautics and Astronautics at RWTH Aachen University. A so-called reference wing (half-span 675mm, solid construction, material: X42Cr13) serves as the measurement object. This half-wing model was to be modified as part of research work. The aim was to investigate the vorticity wake of an aerofoil with the help of this new application in the in-house water circulation channel and in the drag channel of the DST in Duisburg. If successful, the use of this system in practice would offer economic and safety-related advantages for civil aviation. One focus of the design was the development of a transmission gearbox. The bearing of this assembly had to be particularly suitable for use in the water circulation channel without showing signs of corrosion. However, there were a number of other requirements for the bearings. They had to be as small as possible to minimise the impact on the flow, function maintenance-free over a long period of time (no corrosion, insensitive to dust and dirt), be as clearance and vibration-free as possible, generate only a moderate amount of heat and be cost-effective.