A propulsor hub is provided and includes a casing including an inner annular part and blade-connection parts extending outwardly from the inner annular part, a liner having inner and outer opposed radial ends, the liner being disposed about a corresponding one of the blade-connection parts with the inner radial end thereof at a distance from the inner annular part and a weighted element securely disposed about the corresponding one of the blade-connection parts to abut the outer radial end of the liner.
PROPULSOR HUB WEIGHT ELEMENT AND BALANCING METHOD
2018-05-24
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |