| 摘要 |
The invention relates to a rotor blade arrangement (1) for a turbomachine having a blade carrier (9), on whose outer circumferential surface (3) there is formed a circumferential T-shaped slot (4), having a blade ring (5) which comprises a plurality of blades (6) and spacers (8), that are inserted in alternation into the T-shaped slot, and having support elements (9) that are braced between the blades and spacers on one hand and a base (10) of the T-shaped slot on the other hand such that the blades and spacers are pressed radially outward, a separate support element being assigned to each spacer and being releasably held thereon, in particular secured in a clamping manner. The invention also relates to a method for assembling a rotor blade arrangement (1) according to the invention. |
