Circular wing aircraft

Aeronautics and astronautics – Aircraft sustentation

Patent

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Details

244 7A, 244 122, 244 23C, 244 67, 244 73C, B64C 2722, B64C 3906, B64C 2900

Patent

active

055033512

ABSTRACT:
A circular wing aircraft in the form of a helicopter comprising a fuselage and a circular wing assembly. A structure is for mounting the circular wing assembly above the fuselage in a stationary manner. An air impeller unit is rotatively carried within the circular wing assembly. A device is for driving the air impeller unit to rotate about a central axis within the circular wing assembly, so as to provide lift and flight movement while yaw control is maintained.

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