There is disclosed a rotor (3, 3', 3") for an aircraft (1) capable of hovering, comprising: a stationary support structure (10); a rotative element (11), which is rotatable about a first axis (A) with respect to said stationary support structure (10) with a first rotational speed (É2); at least one blade (13), which is operatively connected with said rotative element (11); and a transmission group (37, 37"), which comprises an output element (36, 36', 36") rotatable about first axis (A) with a second rotational speed (É1) different from first rotational speed (É2).
ROTOR FOR AN AIRCRAFT CAPABLE OF HOVERING
ROTOR FÜR EIN SCHWEBEFLUGFÄHIGES LUFTFAHRZEUG
ROTOR POUR UN AÉRONEF CAPABLE DE VOL STATIONNAIRE
2019-07-24
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |