| 摘要 |
The turbine blade (63,65) has a blade element (67,69) arranged along a blade axis (73,75) and a platform region (61) arranged at the foot of the blade and extending transversely with respect to the axis of the blade. The platform is formed by a spring-elastic sheet metal part (77,79) in contact with the blade. An independent claim is also included for a gas turbine with inventive turbine blades. |
