System to reduce the stresses applied in the maintainer group and especially to the root of the wings of an aircraft in flight.

摘要

The present invention concerns a TO DECREASE THE EFFORTS APPLIED TO GROUP BREADWINNER SYSTEM AND IN PARTICULAR TO THE ROOT (1) WINGS (2) OF AN AIRCRAFT (3) in flight, having means (4) SCREENING AND MEASUREMENT OF ACCELERATION VERTICAL AND aIRCRAFT, and means (5) for supplying signals CONTROL SURFACES aerodynamic (6) connected to the wings (2) of the aircraft, driving said control means (5) the angle of deflection aerodynamic said surfaces (6) based on the acceleration signals they receive. According to the invention, said control means (5) are not activated only when said vertical acceleration (TAU) exceeds a threshold DEFAULT (TAU) S.