| 摘要 |
The invention relates to a turbine diffuser (10) for recovering pressure from a fluid exhausted from a last stage blade (8), the diffuser (10). In at least in a region between 10% of the longitudinal length (7) and of the diffuser (10) and a downstream end (11) of the diffuser, the inner guide (12) forms an inflectionless curve and further has a peak radial height at a point between 40%-60% of the longitudinal length (7). |
