Variable gradient control stick force feel adjustment system

Details Variable gradient control stick force feel adjustment system Variable gradient control stick force feel adjustment system

B - Operations, Transporting

64

C

B64C 13/46 (2006.01) B64C 13/12 (2006.01) B64C 13/50 (2006.01) G05D 1/08 (2006.01)

Patent

CA 2380346

A variable gradient control stick force feel adjustment system for use in aircraft is disclosed. A gradient actuator is operationally coupled to at least one spring cartridge assembly in order to move the pivot point of the spring cartridge assembly with respect to the aircraft's directional hardware so that the tension of at least one manual control stick onboard the aircraft can be adjusted. At least one operational parameter input is provided to the gradient actuator from at least one of the aircraft's onboard control devices in order to effect a change in pivot point for the spring cartridge assembly.

L'invention concerne un système de réglage de la sensation d'effort sur le levier à commande de gradient variable utilisable dans un aéronef. Un actionneur de gradient épouse fonctionnellement au moins un ensemble boîtier à ressorts de façon à déplacer le point de pivot dudit ensemble par rapport au matériel directionnel de l'aéronef, ce qui permet de régler au moins un levier de commande manuelle à bord de l'aéronef. L'actionneur de gradient est pourvu d'au moins une entrée de paramètre opérationnel à partir d'au moins un dispositif de commande à bord de l'aéronef, ce qui permet de modifier le point de pivot relatif à l'ensemble boîtier à ressorts.

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