| 摘要 |
The guide vane ring (1) has several rotatable guide vanes (2) with an inner ring (4) for radial inner stabilization of the guide vanes. A seal (44) of the guide vane is adapted to seal the radial clearance formed between inner ring and an opposite rotor portion. The bearing element (6) is adapted to support the guide vanes in the inner ring. Each guide vane is supported in the bearing element. The inner ring is provided with two half rings which are pushed in circumferential direction onto the bearing element. Independent claims are included for the following: (1) method for assembling a guide vane ring; and (2) turbomachine. |
