Electric flight control system for aircraft elevators

Details Electric flight control system for aircraft elevators Electric flight control system for aircraft elevators

G - Physics

05

D

G05D 1/06 (2006.01)

Patent

CA 2567209

The invention relates to an electric flight control system for aircraft elevators. According to the invention, the flight control system can be controlled in terms of load factor or rate of pitch. The inventive system comprises built-in protections in relation to load factor, incidence and pitch attitude.

Selon l'invention, le système de commandes de vol peut être commandé en facteur de charge ou en vitesse de tangage et il comporte des protections intégrées en facteur de charge, en incidence et en assiette longitudinale.

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