ASSERVISSEMENT DU CALAGE DE PALES
ASSERVISSEMENT DU CALAGE DE PALES
- New search for: DENEUVE SÉBASTIEN JEAN FERNAND
- New search for: YING CHARLES
- New search for: DENEUVE SÉBASTIEN JEAN FERNAND
- New search for: YING CHARLES
The invention relates to a method for controlling a pitch angle of the vanes or blades of a propellant body of a turbine engine, comprising generating a pitch command (ifinal) according to a rotational speed of the propeller (XNmes) and a speed setpoint (XNcons), the method comprises a nominal regulating chain (13), wherein the pitch command is further generated according to a value of a pitch angle (βmes) of the vanes or blades of the propellant body, and an off-nominal regulating chain (16), wherein the pitch command is generated independently of a value of a pitch angle of the vanes or blades of the propellant body.
Document information
ASSERVISSEMENT DU CALAGE DE PALES
BLADE PITCH CONTROL
REGELUNG FÜR BLATTVERSTELLUNG
2023-11-22
Patent
Electronic Resource
French