A method for optimizing the operation of at least one first propeller and of at least one second propeller of a hybrid helicopter. The method comprises the following step during a control phase: deflection, with an autopilot system, of at least one aerodynamic stabilizer member into a setpoint position having, with respect to a reference position, a target deflection angle that is a function of a setpoint deflection angle, the setpoint deflection angle being calculated by the autopilot system in order to compensate for a torque exerted by the lift rotor at zero sideslip.
Method for controlling at least one aerodynamic stabilizer member of a hybrid helicopter, and a hybrid helicopter
2023-04-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2021
|METHOD OF CONTROLLING AT LEAST ONE PROPELLER OF A HYBRID HELICOPTER, AND A HYBRID HELICOPTER
European Patent Office | 2021
|Aerodynamic design of the NH90 helicopter stabilizer
Tema Archive | 1997
|METHOD OF CONTROLLING PROPELLERS OF A HYBRID HELICOPTER, AND A HYBRID HELICOPTER
European Patent Office | 2021
|