| 摘要 |
<p>A securing device for blades for gas turbines, of the type used for the first stage of the turbine (with supply of cooling air from the root towards the foil), comprises a plurality of plates (13), each of which is provided with at least one U-shaped projection (19), which can engage with a corresponding U-shaped groove present in the surface of the disc (15) of the first stage of the turbine, such that each of the plates (13) is interposed between two adjacent blades (11), in order to secure them axially. The object of the invention is also a securing device for blades for gas turbines, of the type used for the second stage of the turbine (non-cooled blades), which comprises a plurality of plates, each of which is interposed between the end portion of the foot of a corresponding blade and the turbine disc, and each of which is provided with ends to secure the blade axially. <IMAGE></p> |
