To address the issues of excessive mass flow at surge boundary in the high‑pressure stage and increased surge susceptibility in two‑stage centrifugal compressors,this study investigates the key structural parameter of impeller exit blade angle affecting surge characteristics. Based on CFD numerical simulations validated by the classical Krain impeller model,the influence of exit blade angles in low and high‑pressure stage impellers on overall compressor performance was analyzed. Results show that at the design speed of 70 000 r/min,smaller exit blade angles in both stages improve compressor efficiency at low flow conditions (0.02~0.07 kg/s) with slight pressure ratio reduction. Optimized smaller exit blade angles enhance efficiency by over 3% at low flow rates,reduce surge boundary mass flow by more than 25%,and significantly improve flow stability. The maximum static entropy increase in low and high‑pressure stages decreases by approximately 50% and 25%,respectively,reducing flow losses. This study provides design guidelines for developing two‑stage boosting systems for PEMFC applications.
| 科 Family | 属数 Number of genus | 种数 Number of species | 占总种数比例 Percentage of total species (%) | 属 Genus | 种数 Number of species | 占总种数比例 Percentage of total species (%) |
|---|---|---|---|---|---|---|
| 鹅膏菌科Amanitaceae | 2 | 11 | 5.26 | 鹅膏菌属 Amanita | 10 | 4.78 |
| 小菇科 Mycenaceae | 2 | 12 | 5.74 | 丝盖伞属 Inocybe | 5 | 2.39 |
| 多孔菌科 Polyporaceae | 8 | 14 | 6.70 | 蜡蘑属 Laccaria | 5 | 2.39 |
| 红菇科 Russulaceae | 3 | 23 | 11.00 | 小皮伞属 Marasmius | 6 | 2.87 |
| 小菇属 Mycena | 11 | 5.26 | ||||
| 光柄菇属 Pluteus | 5 | 2.39 | ||||
| 红菇属 Russula | 17 | 8.13 | ||||
| 栓菌属 Trametes | 5 | 2.39 |