An anti-torque system (10) for a helicopter (1) is described that comprises: an electric power supply unit (15); at least one first rotor (17), operatively connected to an electric power supply unit (15) and operable by the electric power supply unit (15) so as to rotate with a first variable angular speed; and at least one second rotor (25) operatively connected to electric power supply unit (15) and operable by the electric power supply unit (15) so as to rotate with a second variable angular speed.
HELICOPTER WITH AN ANTI-TORQUE SYSTEM
HUBSCHRAUBER MIT EINEM ANTI-DREHMOMENTSYSTEM
HÉLICOPTÈRE AVEC UN SYSTÈME ANTICOUPLE
2022-09-28
Patent
Electronic Resource
English