The invention is related to a pitch control device (14) for a ducted tail rotor of a rotorcraft. The pitch control device (14) comprises a control input member (16) with a disc-shaped central component (16a) and at least two connecting arms (16b) that extend radially from the disc-shaped central component (16a), wherein the disc-shaped central component (16a) is provided for being mounted to an associated pitch control shaft of the ducted tail rotor, and a control transfer member (15) with a ring-shaped connector (15a) and at leas two push rods (15b) that extend axially from the ring-shaped connector (15a), wherein each one of the at least two push rods (15b) is provided for being coupled to an associated pitch lever of a rotor blade of the ducted tail rotor.
PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT
ANSTELLWINKELSTEUERUNGSVORRICHTUNG FÜR EINEN HECKROTOR EINES DREHFLÜGLERS
DISPOSITIF DE COMMANDE DE PAS POUR UN FENESTRON D'UN GIRAVION
2019-04-17
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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