Aircraft pitch control systems and methods are disclosed. An aircraft pitch control system (28) comprises a movable horizontal stabilizer (24) and an elevator (26) movably coupled to the horizontal stabilizer. The elevator is electronically geared to the horizontal stabilizer.
L'invention concerne des systèmes et des procédés de commande de pas d'aéronef. Un système de commande de pas d'aéronef (28) comprend un stabilisateur horizontal mobile (24) et un élévateur (26) couplé de façon mobile au stabilisateur horizontal. L'élévateur est couplé électroniquement au stabilisateur horizontal.
AIRCRAFT PITCH CONTROL SYSTEM WITH ELECTRONICALLY GEARED ELEVATOR
SYSTEME DE COMMANDE DE PAS D'AERONEF AVEC ELEVATEUR A ENGRENAGE ELECTRONIQUE
2017-11-02
Patent
Electronic Resource
English
AIRCRAFT PITCH CONTROL SYSTEM WITH ELECTRONICALLY GEARED ELEVATOR
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