A propeller assembly (10) for aircrafts has a hub (12) having at least one receiver opening (16), a receiver (18) located within the receiver opening (16) and having a first collar (20) defining a blade opening (22), a blade (14) having a second collar (24) and a protrusion (26) with the second collar (24) abutting the first collar (20) and the protrusion (26) received within the blade opening (22), and a first retainer (32), and a second retainer (40).
PROPELLER ASSEMBLY AND PROPELLER BLADE RETENTION ASSEMBLY FOR AIRCRAFTS
2015-04-15
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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