REPAIR MEMBER FOR A VANE ASSEMBLY OF A GAS TURBINE AND METHOD FOR REPAIRING A DAMAGED VANE OF A VANE ASSEMBLY OF A GAS TURBINE
The repair member includes an inner platform, an outer platform portion, and an airfoil portion connecting the inner and outer platform portions; the inner platform portion is configured so to reach an edge of a first ring or sector of ring of a vane assembly of the damaged vane, and the outer platf...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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