A direct orientation vector rotor (DOVER) for use on rotary wing aircraft includes a gear set for multidirectional rotor orientation based on the spherical coordinate system; an inclination mechanism, wherein the rotor is moved from the 0° horizontal position to an inclined position; a rotational turret, wherein the rotor is moved along the azimuth and wherein the inclination mechanism is housed; and a motion-adapted gear lubrication housing.
DIRECT ORIENTATION VECTOR ROTOR (DOVER)
ROTORVEKTOR MIT DIREKTER AUSRICHTUNG
ROTOR DE VECTEUR D'ORIENTATION DIRECTE
15.07.2020
Patent
Elektronische Ressource
Englisch
Online Contents | 1997
|British Library Online Contents | 1997
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