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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
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
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机译:燃气轮机叶片总成的维修件及维修方法
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摘要
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 platform portion is configured so to reach an edge of a second ring or sector of ring of the a vane assembly of the damaged vane; the inner platform portion, the outer platform portion, and the airfoil portion are configured so to allow insertion of the repair member into the vane assembly by a pure translation movement being along an insertion direction and having a movement component parallel to an axes of the first and second rings or sectors of ring.
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