| 摘要 |
A method of fabrication of aerodynamic profiles for aerogenerator or aerodyne blades and the blade thus obtained, which consists of the covering separately of moulds or mandrels (2) with composites of fibres impregnated with synthetic resins, so that later and once these mandrels (2) have been covered they may be joined together by means of transversal fixings (12), the assembly thus formed being arranged between two layers (15 and 16), also formed from a composite of fibres impregnated with synthetic resins, with the arrangement of all this between a pair of moulds (3 and 4), in order to conclude with a method of curing by which is obtained a monocoque profile determining the general body of the corresponding blade.
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