Electrical control system for an aircraft steering vane

Details Electrical control system for an aircraft steering vane Electrical control system for an aircraft steering vane

B - Operations, Transporting

64

C

B64C 13/50 (2006.01)

Patent

CA 2640521

The invention concerns a system (1) comprising a steering vane (2) which can turn within a rudder deflection range which is limited by first and second rudder deflection limits, and means (12) for asymmetrically varying said first and second rudder deflection limits based on the current values of the aircraft flight parameters.

Le système (1) comporte une gouverne de direction (2) qui peut tourner à l'intérieur d'une plage de débattement qui est limitée par une première et une seconde limites de débattement, et un moyen (12) pour varier lesdites première et seconde limites de débattement, de façon dissymétrique, en fonction de valeurs courantes de paramètres de vol de l'avion.

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