A flexbeam unit for a multi-blade rotor of a rotary wing aircraft, the flexbeam unit comprising a plurality of flexbeam elements defining a predetermined number of torsion elements that are connectable with associated rotor blades of the multi-blade rotor, at least one of the predetermined number of torsion elements comprising at least one flexbeam element having an associated longitudinal direction, the at least one flexbeam element comprising at least one twisted area in which the at least one flexbeam element is twisted in the associated longitudinal direction.
Flexbeam unit with at least one twisted flexbeam element
2018-06-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
FLEXBEAM UNIT WITH AT LEAST ONE TWISTED FLEXBEAM ELEMENT
European Patent Office | 2015
|Flexbeam unit with at least one twisted flexbeam element
European Patent Office | 2018
|Partly cruciform flexbeam and method of manufacturing such a flexbeam
European Patent Office | 2016
|Partly cruciform flexbeam and method of manufacturing such a flexbeam
European Patent Office | 2017
|