An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes.
IMPACT RESISTANT PROPELLER SYSTEM
SCHLAGFESTES PROPELLERSYSTEM
SYSTÈME DE PROPULSION RÉSISTANT AUX CHOCS
11.11.2020
Patent
Elektronische Ressource
Englisch
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