A fixed-wing VTOL aircraft (100) with a rotor assembly (110). The rotor assembly (110) is configured to provide vertical flight for the fixed-wing VTOL aircraft (100). The rotor assembly (110) includes a hub assembly (602), a first rotor blade (605) affixed to the hub assembly (602), and a second rotor blade (604) affixed to the hub assembly (602). The hub assembly (602) orients the second rotor blade (604) in relation to the first rotor blade (605) about an axis of rotation of the hub assembly (602) with the first rotor blade (605) and the second rotor blade (604) vertically stacked when the hub assembly (602) is stopped for wing-borne flight.
FOLDABLE ROTOR ASSEMBLY FOR FIXED-WING VTOL AIRCRAFT
KLAPPBARE ROTORANORDNUNG FÜR STARRFLÜGEL-VTOL-LUFTFAHRZEUGE
ENSEMBLE DE ROTOR PLIABLE POUR AVION À DÉCOLLAGE ET À ATTERRISSAGE VERTICAUX À VOILURE FIXE
2020-08-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Engineering Index Backfile | 1957
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