| 摘要 |
A turbine blade/vane includes a profiled blade/vane aerofoil, which extends along a blade/vane axis to be capable of absorbing high thermal and mechanical loading, on the one hand, and to ensure a comparatively economical consumption of coolant, on the other. For this purpose, the blade/vane aerofoil includes, integrally formed on it, a hot-gas platform extending transversely to the blade/vane axis and, above it, a load platform. A mechanical connection between the load platform and the hot-gas platform occurs exclusively by way of the blade/vane aerofoil.
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