| 摘要 |
The invention concerns a land and flying vehicle with its tubular frame, 2 main rotors with triangular blades and adjustable pitch-propellers, with its drive propelled by the force of a hydraulic turbine located at the end of its driving shaft. Said force is propelled by a hydraulic pump THP driven by an internal combustion engine or reactor. Streamlined pusher propellers (14) (already patented) located on the side (Fig. 2) are driven by hydraulic turbines located at the shaft end of rotating propellers (14) once they are extended from 0 DEG to 180 DEG . Streamlined pitch blades (13) with collective opening are located under the 2 passenger seats and provide stability. The pilot is in the centre, above the engine and the air-driven pump. All the driving hydraulic systems are located at the shaft ends and enable said manoeuvres. The drawings (Fig. 3, Fig. 4, Fig. 5) describe the revolutionary design and enable the installation of said system on some current helicopter models. By said method the present drive assembly, gimbal joints, gear-boxes are replaced with turbine drives with smooth and lightweight start. Said methods can be adapted on running vehicles, including trains, whereof the designs and applications are reserved.
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