A helicopter has a mast axis and a rotorcraft blade assembly (100). The rotorcraft blade assembly (100) has a main body (102) and a blade tip (104) movable relative to the main body (102). The rotorcraft blade assembly (100) is selectively rotatable about the mast axis.
VARIABLE SWEEP ROTORCRAFT BLADE TIP
ROTORBLATTSPITZE EINES DREHFLÜGELFLUGZEUGES MIT VARIABLER SCHWENKBEWEGUNG
POINTE DE LAME DE GIRAVION À BALAYAGE VARIABLE
28.08.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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