| 摘要 |
<p>The system (22) has multiple axial safety elements (24) that are provided with two sections with different profile regions (26a,26b), where each profile region is provided for arrangement between a groove bottom (14a,14b) of a rotor shaft (10) and a blade root (6a,6b). The two sections are connected to each other by a connecting rod and are positioned in groove spacing. The blade-side counter-contours (28a,28b) are provided for the respective formation of a form-fitting pair with the profile regions. The enlarged locking portions are formed radially outward against end face of the blade root. Independent claims are also included for the following: (1) a turbo-machine with a rotor; and (2) a method for manufacturing a rotor of a turbo machine.</p> |
