초록 ▼

A method for preventing vibration of a rudder of an aircraft may have, on a lateral aerodynamic surface of the aircraft's rudder, a protruding aerodynamic element capable of generating an aerodynamic effect tending to rotate the rudder about its articulation axis. An actuator of the rudder is contro

A method for preventing vibration of a rudder of an aircraft may have, on a lateral aerodynamic surface of the aircraft's rudder, a protruding aerodynamic element capable of generating an aerodynamic effect tending to rotate the rudder about its articulation axis. An actuator of the rudder is controlled such that it counters the action of the protruding aerodynamic element and such that it imposes on the rudder a position of equilibrium in aerodynamic extension of the fixed vertical stabilizer.

대표청구항 ▼

The invention claimed is: 1. A method for preventing vibration of a rudder of an aircraft flying without sideslip, said rudder being connected to a fixed vertical stabilizer by an articulation section that forms an articulation axis, being able to rotate about said articulation axis under the actio

The invention claimed is: 1. A method for preventing vibration of a rudder of an aircraft flying without sideslip, said rudder being connected to a fixed vertical stabilizer by an articulation section that forms an articulation axis, being able to rotate about said articulation axis under the action of a controllable actuator, and comprising two lateral aerodynamic surfaces meeting at the rear end of the aircraft in order to form a trailing edge, said vibration resulting from mechanical plays in said articulation section or in a transmission section that connects said controllable actuator and said rudder, wherein said method comprises the steps of: fixing a protruding aerodynamic element on one of said lateral aerodynamic surfaces of the rudder, said protruding aerodynamic element being capable of generating an aerodynamic effect tending to rotate said rudder about said articulation axis; and controlling said actuator for countering said aerodynamic effect of said protruding aerodynamic element for imposing on said rudder a position of equilibrium in aerodynamic extension of said fixed vertical stabilizer, wherein: said control for imposing on said rudder the position of equilibrium prevents said rudder vibrations resulting from said mechanical plays, and said protruding aerodynamic element is fixed in a temporary manner onto said rudder when said mechanical plays are at a first level and is removed from said rudder when said mechanical plays are below said first level. 2. The method as claimed in claim 1, wherein said protruding aerodynamic element is fixed in the vicinity of the trailing edge of said rudder. 3. The method as claimed in claim 1, further comprising fixing said protruding aerodynamic element on said one of said lateral aerodynamic surfaces by complementary attachment elements some of which are fixed permanently on said mobile rudder. 4. The method as claimed in claim 1, further comprising using complementary attachment elements comprising screws and nuts and wherein one incorporates said nuts in said one of said lateral aerodynamic surfaces. 5. The method as claimed in claim 1, further comprising using a protruding aerodynamic element having an elongated shape and wherein one disposes it, on said one of said lateral aerodynamic surfaces, in a way that is at least approximately parallel with the trailing edge of said rudder. 6. The method as claimed in claim 4, further comprising using a protruding aerodynamic element which is a length of angle section fixed by one of its flanges to said one of said lateral aerodynamic surfaces, the other flange of said length of angle section protruding with respect to said one of said lateral aerodynamic surfaces.