A rotor comprising a hub and a plurality of lift assemblies. Each lift assembly is connected to two adjacent lift assemblies respectively by a first damper and a second damper. The first damper is hinged to a lift assembly about a first axis, and the second damper is hinged to said lift assembly about a second axis. A first plane contains a lead-lag axis of the lift assembly and orthogonally to the pitch axis of the lift assembly. The first axis is situated in a volume lying between the first plane and an axis of rotation of the rotor, the second axis being positioned outside said volume.
ROTOR ET AERONEF POURVU D'UN TEL ROTOR
A ROTOR AND AN AIRCRAFT PROVIDED WITH SUCH A ROTOR
ROTOR UND MIT EINEM SOLCHEN ROTOR AUSGESTATTETES LUFTFAHRZEUG
28.11.2018
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
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