A pitch control device for a ducted tail rotor of a rotorcraft. The pitch control device comprises a control input member with a disc-shaped central component and at least two connecting arms that extend radially from the disc-shaped central component, wherein the disc-shaped central component is provided for being mounted to an associated pitch control shaft of the ducted tail rotor, and a control transfer member with a ring-shaped connector and at least two push rods that extend axially from the ring-shaped connector, wherein each one of the at least two push rods 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
2020-05-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT
European Patent Office | 2019
PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT
European Patent Office | 2019
|PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT
European Patent Office | 2018
|PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT
European Patent Office | 2018
|PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT
European Patent Office | 2019
|