Mechanical flight control auxiliary power assist system

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 41/00 (2006.01)

Patent

CA 2580276

A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and a booster means for connecting the upstream portion to the downstream portion. The booster means may comprise dual concentric valve actuators and/or a variety of system load limiting features.

L'invention concerne un système à commande de vol mécanique destiné à un aéronef à voilure tournante. Le système à commande de vol comprend une partie en amont, une partie en aval, et un élément de relais destiné à connecter la partie en amont à la partie en aval. L'élément de relais peut comprendre des actionneurs de soupape concentrique double et/ou une variété de caractéristiques de limitation de charge système.

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