The present invention provides an aircraft described as an Airborne Urban Mobility Vehicle with VTOL (Vertical Take-Off and Landing) capability. The aircraft has a 5 fuselage freely pivoted between lateral arms of a yoke; the arms of the yoke extending fore and aft and, at or towards the extremities of the arms: the respective fore portions are linked laterally together by an aerofoil; and the respective aft portions are linked laterally together by an aerofoil; and at least one of the fore and aft aerofoils having mounted thereon one or more propulsion units.
TANDEM WING TAIL-SITTING AIRCRAFT WITH TILTING BODY
08.10.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
A TANDEM WING TAIL-SITTING AIRCRAFT WITH TILTING BODY
Europäisches Patentamt | 2019
|Tandem wing tilting rotor aircraft and aircraft manufacturing method
Europäisches Patentamt | 2020
|VTOL TAIL SITTING AIRCRAFT WITH ROTOR BLOWN NONPLANAR WING CONFIGURATION
Europäisches Patentamt | 2022
|Composite tilting wing tandem autorotation double-rotor aircraft
Europäisches Patentamt | 2020
|Composite tilting wing tandem variable-wing reverse-speed rotor aircraft
Europäisches Patentamt | 2020
|