| 摘要 |
<p>A current-generating self-supported aerial apparatus for high- altitude winds is described, which comprises: a fuselage (1) on which two pairs of wings (2, 2b) are assembled, one wing on the front side and one wing on the rear side of the fuselage (1); behind the wings (2, 2b), turbines are assembled of a cylindrical fan type, these turbines covering the whole wing length; electric motors (9, 9b) adapted to actuate the turbines and to operate as generators when the turbines are moved by wind; wing drifts (5) on which the electric motors (9, 9b) are assembled; wing ailerons (6) and tail ailerons (3) for stabilizing the apparatus; an electronic managing system for the apparatus; means for rotating the turbine scrolls (13); and emergency parachute means (10b).</p> |
