A propeller blade arrangement comprising a propeller blade (10) attached to and rotatable with a hub (30), via a retention bearing (20), the blade (10) being rotatable about a center line of the blade (10), the retention bearing (20) configured to tilt the blade (10) such that its center line is tilted with respect to the hub (30).
PROPELLER BLADE ARRANGEMENT
PROPELLERBLATTANORDNUNG
AGENCEMENT DE PALE D'HÉLICE
2021-09-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |