| 摘要 |
<p>Disclosed is a turbine blade (1) with a blade root (2), an aerofoil (4), at least one cooling passage (5) arranged in the turbine blade (1) and extending from the blade root (2) to the aerofoil (4), and a liner (6) arranged in the at least one cooling passage (5) for protecting the cooling passage 10 (5) against corrosion, especially type II hot corrosion.</p> |
