| 摘要 |
The present invention relates to a turbine blade which includes a route portion which slides to be accommodated when installing slots of an airfoil, a platform, and a rotor disk. The blade is disposed on the route portion to fix the blade in an axial direction with respect to the rotor disk and additionally includes a locking member coupled to the rotor disk. A blade having a simple and cost-efficient axial locking system is provided to axially fix the blade with respect to the rotor disk. Also, a fail safe solution during an assembly process is provided. |
