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
2019-08-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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