TANDEM WING TAIL-SITTING AIRCRAFT WITH TILTING BODY

摘要

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.