AERODYNAMIC BODY, AND ALSO A WING WITH AERODYNAMIC BODY, COMBINATION OF A COMPUTER AND WING OR AERODYNAMIC BODY, METHOD OF INFLUENCE ON THE CONTROL SIGNALS FOR A COMPUTER SERVICE SYSTEM AND A COMPUTER SERVICE DRIVER

摘要

1. Aerodynamic body (4) for mounting on a wing, characterized in that at least two flaps (5a, 5b) are located at the downstream end of the aerodynamic body (4). ! 2. The aerodynamic body (4) according to claim 1, characterized in that the flaps (5a, 5b) are located directly next to each other with respect to the longitudinal direction of the aerodynamic body (4)! 3. The aerodynamic body according to claim 1, characterized in that between the flaps (5a, 5b) located on the aerodynamic body (4) is a structural part. ! 4. The aerodynamic body according to claim 1, characterized in that the dimensions of at least two aerodynamic bodies (4) are selected so that when oscillating with a phase shift of at least two flaps (5a, 5b), the aerodynamic forces induced by this movement in any point in time is less than 10% of the maximum aerodynamic force that can be induced by one flap. ! 5. The aerodynamic body (4) according to claim 1, characterized in that during the antiphase oscillation of at least two flaps, the aerodynamic forces induced by the movement of these aerodynamic bodies (4) mutually cancel at any point in time of the oscillation period. ! 6. The aerodynamic body (4) according to claim 1, characterized in that the flaps (5a, 5b) of the aerodynamic body (4) are provided with at least one servo drive, which is configured to rotate at least one flap from the zero position. ! 7. The aerodynamic body (4) according to claim 6, characterized in that the aerodynamic body (4) includes a computer for actuating at least one servo drive. ! 8. Aerodynamic body (4) according to claim 1, characterized in that at least two