Method and device for attenuating on an aircraft the effects...

G - Physics – 05 – D

Patent

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G05D 1/06 (2006.01) B64C 13/16 (2006.01)

Patent

CA 2622110

The invention concerns a device (1) comprising means (4) for determining automatically, using a vertical wind component, a level of severity concerning a vertical turbulence, and means (5) for computing automatically, using said vertical wind component, a control instruction for a controllable member (2), which enables the amplitude of load factors generated on the aircraft by the vertical turbulence to be minimized.

Le dispositif (1) comporte des moyens (4) pour déterminer automatique ment, à l'aide d'une composante verticale du vent, un niveau de sévérité concernant une turbulence verticale, et des moyens (5) pour calculer automatiquement, à l'aide de cette composante verticale du vent, un ordre de commande pour un organe mobile commandable (2), qui permet de minimiser l'amplitude des facteurs de charge engendrés sur l'aéronef par la turbulence verticale.

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