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Aircraft, has circular wings arranged in air channels, where air is reduced over upper surfaces of upper sphere for forming additional buoyancy when ventilator system or turbo-blower system or other drive systems is operated
Aircraft, has circular wings arranged in air channels, where air is reduced over upper surfaces of upper sphere for forming additional buoyancy when ventilator system or turbo-blower system or other drive systems is operated
The aircraft (20) has circular wings (2, 3, 6) arranged in air channels (17), where the wings are attached at an incident angle. An upper sphere (7) and a lower sphere (9) cut the air channels to each other at a preset angle or at null such that elevons expand area of potentials of the aircraft, and a thrust vector is rapidly changed in an opposite position for emergency braking during maneuvers. Air is reduced over upper surfaces of the upper sphere for forming additional buoyancy when a ventilator system or turbo-blower system or other drive systems is operated.
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