Control systems (20) for a rotorcraft (1) are provided, the rotorcraft (1) including main rotor (5) and auxiliary propulsor assemblies (6). the main rotor assembly (1) including first (50) and second (51) rotors disposed to oppositely rotate relative to an airframe (2) about a same rotational axis (RA), and sensors (30) disposed to generate hub moment, tip clearance and lift offset data of the main rotor assembly (5).
LIFT OFFSET MANAGEMENT AND CONTROL SYSTEMS FOR COAXIAL ROTORCRAFT
LIFT-OFFSET MANAGEMENT UND STEUERUNGSSYSTEME FÜR KOAXIALE HUBSCHRAUBER
GESTION DE DÉCALAGE DE LEVAGE ET SYSTÈMES DE COMMANDE POUR GIRAVION COAXIAL
2018-10-24
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Lift offset management and control systems for coaxial rotorcraft
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