| 摘要 |
<p>The invention relates to an apparatus that can be propelled and exploited in various fluids and which, during motion, overcomes the fluid resistance by rotation. According to the invention, the aircraft comprises a spheroidal-disc-shaped body (1) to which there is articulated a turbine assembly (2) and which is coupled with a complex of concentric axles (3) by means of a periaxial collar (14), the turbine assembly (2) comprising three turbines (18, 21 and 22), namely an upper turbine, an intermediate one and a lower turbine, all of them being provided with some fluid intake blades (44), the complex of axles (3) consisting of a central axle (26) concentrically placed within an external axle (27).</p> |
