Vertical take off and landing aircraft

摘要: An aircraft for vertical take off and landing is comprised of a rotor assembly mounted on rotating drive shaft extending from the top cabin. The truncated-cone top, spaced apart circular bottom, internal vanes running radially, between forming an air impeller. In operation, drawn through central intake discharged annular nozzle around circumference assembly. As rotates, additional rammed scoops at angle to radii surface top. torque applied cabin, due rotation by engine assembly, countered reaction force generated plurality tabs cabin sidewall into airstream flowing downwardly nozzle.