A propeller assembly including a shaft having a rotational axis; a plurality of propellers connected to the shaft; means for deploying the plurality of propellers using a centrifugal force generated from a rotation of the shaft, so as to provide vertical thrust during a vertical take-off and landing of the aircraft; and means for restoring the propellers into a stowed configuration.
SCISSORING PROPELLER WITH CENTRIPETALLY ACTUATED CENTERING LEVER LOCK
2021-10-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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