Vertical take off and landing aircraft has three propellers mounted at wing tips and on tail respectively

摘要

The vertical take off and landing aircraft has three steerable propellers (H1-3) positioned in a triangular array. Two propellers are mounted on a support perpendicular to the longitudinal al axis of the fuselage of the aircraft and the other is mounted on the tail. The propellers are driven by a hydraulic motor (2a-c) driven by a central power source (2) driven by a Diesel or turbine.