The invention is related to a multi-blade rotor (1) for a rotary wing aircraft, comprising a plurality of rotor blades (2a - 2e) connected to an associated rotor head (3) via a plurality of flexbeam elements (10a - 10e), wherin at least one flexbeam element (10a - 10e) of the plurality of flexbeam elements (10a - 10e) comprises an asymmetrical flexbeam root (14a - 14c) that is mounted to the associated rotor head (3).
MULTI-BLADE ROTOR FOR A ROTARY WING AIRCRAFT
MEHRBLATTROTOR FÜR EIN DREHFLÜGELFLUGZEUG
ROTOR À PALES MULTIPLES POUR UN AÉRONEF À VOILURE TOURNANTE
2019-07-03
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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