A rotorcraft rotor blade assembly (100) includes an upper skin portion (104) extending substantially a full span of the rotor blade assembly (100) and a lower skin portion (106) extending substantially the full span of the rotor blade assembly (100). Each of the upper skin portion (104) and the lower skin portion (106) is configured to carry at least substantially 30% of rotor blade assembly (100) loads.
ROTORCRAFT ROTOR BLADE ASSEMBLY
ROTORBLATTANORDNUNG EINES DREHFLÜGELFLUGZEUGS
ENSEMBLE PALE DE ROTOR D'UN GIRAVION
2018-12-05
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |