The present invention includes an a plurality of first variable speed motors (112a -112i) arranged in a first matrix pattern and mounted on a tail boom (108) of the helicopter (100); one or more fixed pitch blades attached to each of the plurality of first variable speed motors (112a - 112i); and wherein a speed of one or more of the plurality of first variable speed motors (112a - 112i) is varied to provide an anti-torque thrust.
ANTI-TORQUE CONTROL USING MATRIX OF FIXED BLADE PITCH MOTOR MODULES
DREHMOMENTAUSGLEICHSSTEUERUNG UNTER VERWENDUNG EINER MATRIX VON MOTORMODULEN MIT STARRER BLATTSTELLUNG
COMMANDE ANTI-COUPLE UTILISANT UNE MATRICE DE MODULES DE MOTEUR DE PAS DE PALE FIXE
2018-12-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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