| 摘要 |
The present invention describes a vertical aeromotor comprising e vanes with r reinforcements (Figures 2, 2', 2'', 4 and 5), said e vanes being elongated and having a 70 degree angular configuration. In Figure 1, section A, the assembly of two e vanes with r reinforcements is shown, said e vanes being disposed in a completely opposite relationship with each other, and joined by a c tie rod at each of the ends of one of the smallest sides thereof to a main axle, by means of a t pilot screw, to support rotary stress of the e vanes. Said e vanes, as illustrated on Figures 2' and 2'', are joined together by means of the c tie rod each by one of the ends thereof to the f axle and by the end of the adjacent e vane and, as shown on Figures 4 and 5, they are joined by one of their ends both to the f axle as well as to other of said e vanes, by a single c tie rod, on those same sides, and said e vanes are also joined by their far ends from f axle through c tie rods both to one of their ends as well as to its angular vertex, thus forming a 360 degree configuration. These e vanes are capable of being easily assembled and dissembled and they are constituted of resistant structural material, which provides rigidity and lightness and can be turned over upside down or vice versa, to obtain a turn change in vertical aeromotor, as desired. Each e vane can be constituted by two elongated rectangular sections longitudinally joined in angular form, with reinforcements, or can be formed by two rectangular sections joined together in a longitudinal way by means of hinges, Figure 6, so that this last type of vane with hinges can be opened and closed in a repetitive way. Vertical aeromotor also comprises a h ball bearing arrangement to support e vanes and f axle weight inside a g cylinder; and a i base cylindrical section or vertical aeromotor general support, g cylinder being coupled to i cylindrical section, which has a diameter larger than said g cylinder.
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