A vertical take-off and landing (VTOL) aircraft is provided. The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors being rotatable to generate lift in vertical flight and thrust in horizontal flight and a delta-wing shaped fuselage disposed along the wing between the nacelles.
Delta fuselage for vertical take-off and landing (VTOL) aircraft
2020-01-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
DELTA FUSELAGE FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT
European Patent Office | 2017
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