The present invention includes an anti-torque assembly (110) for a helicopter (100) comprising a plurality of fixed blade pitch motors (112a-g) mounted on one or more pivots on the tail boom (108) of the helicopter (100), wherein the plurality of fixed blade pitch motors on the one or more pivots are adapted to be oriented substantially in-plane with a tail boom (108) of a helicopter (100) during a first mode of operation that comprises a hover mode and wherein the fixed blade pitch motors (112a-g) are adapted to be oriented substantially off-plane from the tail boom (108) of the helicopter (100) during a second mode of helicopter operation that is different from the first mode.
VARIABLE DIRECTIONAL THRUST FOR HELICOPTER TAIL ANTI-TORQUE SYSTEM
VARIABLER DIREKTIONALER SCHUB FÜR HUBSCHRAUBER-HECKDREHMOMENTAUSGLEICHSSYSTEM
POUSSÉE DIRECTIONNELLE VARIABLE POUR SYSTÈME ANTICOUPLE DE QUEUE D'HÉLICOPTÈRE
2020-01-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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