There is disclosed a rotor for an aircraft capable of hovering, comprising: a stationary support structure; a rotative element, which is rotatable about a first axis with respect to said stationary support structure with a first rotational speed; at least one blade, which is operatively connected with said rotative element; and a transmission group, which comprises an output element rotatable about first axis with a second rotational speed different from first rotational speed.
ROTOR FOR AN AIRCRAFT CAPABLE OF HOVERING
2019-11-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |