G - Physics – 05 – D
Patent
G - Physics
05
D
G05D 1/08 (2006.01)
Patent
CA 2664103
One embodiment of the present invention is a method for automatically reducing the effect of a component of an external force that is laterally incident on a rotorcraft. A signal of the rotorcraft indicative of and proportional to the component is monitored. An absolute value of the signal and a preset high limit are compared. If the absolute value is greater than the preset high limit, manual heading control of the rotorcraft is disabled and the heading of the rotorcraft is adjusted with respect to the external force so as to decrease the lateral component of the external force experienced by the rotorcraft.
Un mode de réalisation de la présente invention concerne un procédé pour réduire automatiquement l'effet de la composante d'une force externe et incidente latéralement sur un giravion. Le signal du giravion indicatif de la composante et proportionnel à celle-ci est surveillé. Une valeur absolue du signal et une limite haute préétablie sont comparées. Si la valeur absolue est supérieure à la limite haute préétablie, un contrôle de CAP manuel du giravion est interdit, et le CAP du giravion est ajusté par rapport à la force externe de manière à diminuer la composante latérale de la force externe subie par le giravion.
Bell Helicopter Textron Inc.
Builta Kenneth E.
Graham Lorelei G.
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