A method of controlling at least one first propeller of a hybrid helicopter, the hybrid helicopter having a thrust control for controlling a first pitch of the first blades of the first propeller. The thrust control includes a movable control member. The method includes the following steps: the thrust control continuously transmitting a control signal carrying a control setpoint to the control system; the control system transforming the control setpoint into a pitch setpoint; and the control system controlling the first pitch by applying the pitch setpoint.
METHOD OF CONTROLLING AT LEAST ONE PROPELLER OF A HYBRID HELICOPTER, AND A HYBRID HELICOPTER
2021-09-23
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2021
|METHOD OF CONTROLLING PROPELLERS OF A HYBRID HELICOPTER, AND A HYBRID HELICOPTER
European Patent Office | 2021
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