• Patentinformation on request

Movie 1

The cascaded turbine is equipped with fixed annular guide vanes to influence the inlet of circular blades. The circular blade of the ring-shaped rotor is thus struck at an inclined angle to the axis of rotation, so that it provides thrust in the direction of flight. The cascaded turbine has a ring blade fan and several successive stages as a secondary modules. The airplane has a new maneuvering system by changing the distance between nose and tail sided hinges the angle of attack changes in opposite directions at front and rear wings to enable the aircraft to maneuver accurately.



  • Patentinformation on request

Movie 2