| 摘要 |
PURPOSE:To enable a turbine to be transported in an integrated configuration by screwing a rotor antirotation bolt in a tapped hole for the spindle of a rotor through a hole of the packing casing of a gland part and inserting and fixing a cushioning material in a clearance between said casing and said rotor. CONSTITUTION:A rotor antirotation bolt 10 is screwed and fixed in a tapped hole 16 for a balancing regulating spindle of a rotor 5 through the hole 15 of a packing casing 7 when transportation of integrated configuration is performed, in regard to a turbine gland part for attaching said casing 7 of labyrinth packing to the end part of a casing 6. And a cushioning material 12 with which a clearance to the rotor 5 is filled is inserted in a space of the end part of of the packing casing 7 formed after a removal of labyrinth packing. Further, the cushioning material 12 is fixed to the end face of the packing casing 7 to secure a rotor push plate 11 for stopping axial movement of the rotor 5. Accordingly, damage of inner parts can be prevented during integrated transportation.
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