A rotary system including a grip having an opening forming a first bridge for receiving a centrifugal force bearing that faces inwardly towards the rotor mast. A rotor blade couples to the grip and a pitch horn positioned outside the opening pitches the rotor blade during flight. A bearing assembly attaches the first bridge to the yoke and controls blade forces exerted against the hub assembly during flight.
Articulated main rotor hub with inwardly CF bearing and 3% flapping hinge offset
2017-09-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Articulated main rotor hub with inwardly CF bearing and 3% flapping hinge offset
European Patent Office | 2019
|ARTICULATED MAIN ROTOR HUB WITH INWARDLY CF BEARING AND 3% FLAPPING HINGE OFFSET
European Patent Office | 2015
|Articulated Main Rotor Hub with Inwardly CF Bearing and 3% Flapping Hinge Offset
European Patent Office | 2018
|Online Contents | 2008
High Offset Flapping Pin Rotor Analysis
Emerald Group Publishing | 1954
|