| 摘要 |
A rotor end piece ( 1 ) for a rotor ( 6 ) of a thermal turbomachine, having at least one circumferential slot ( 3 ) in which moving blades and intermediate pieces are provided, includes a residual gap ( 15 ) formed between an end blade ( 2 ) and an end part ( 11 ), in which residual gap ( 15 ) two end piece halves ( 4, 4 ) are arranged which have securing tabs ( 8, 8 ) which are in each case connected to the latter in one piece and are in engagement with the end blade ( 2 ) and with the end part ( 11 ), respectively.
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