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Influence of Rotor Blade Stagger Angle on Rotating Stall Inception in an Axial-Flow Fan

机译:轴流风扇动叶片错位角对旋转失速开始的影响

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Pressure fluctuations on the casing wall of an axial flow fan were measured. These measure- ments were used to investigate the inception of rotating stall at different rotor-blade stagger angles. Near the peak of the pressure rise, stall cells formed around blades with the design stagger angle as well as around blades with a larger stagger angle. When flow rate was decreased, the stall cells were developed in the case of the design stagger angle, but not developed in the case of the larger stagger angle. Rotating stall was not observed in the case of a smaller stagger angle untill the flow rate was much lower than that at the peak pressure rise. It was confirmed that the formation and development of stall cells were affected by the throat length of the rotor blade passage and the pressure fluctuation magunitude.
机译:测量了轴流风扇的壳体壁上的压力波动。这些测量用于研究在不同的转子叶片错开角度下旋转失速的开始。在压力上升的峰值附近,在具有设计交错角的叶片周围以及在具有较大交错角的叶片周围形成失速单元。当流速降低时,在设计错位角的情况下会产生失速单元,而在错位角较大的情况下不会产生失速单元。在较小的错位角的情况下,没有观察到旋转失速,直到流速远低于峰值压力上升时的流速。证实了失速单元的形成和发展受转子叶片通道的喉长和压力波动程度的影响。

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