摘要

The feature of tip-leakage vortex breakdown and the stability mechanism were analyzed and summarized using the first-stage rotor blade of GE-E3turbine. The study indicated that: the breakdown of tip-leakage vortex core was caused by vortex's centrifugal instability;the vortex core expanded rapidly after losing stability and reversed flow was formed;the vortex core stability depended on two factors: swirling number and reversed pressure gradient. After that, the control of tip-leakage loss was carried out from the perspective of vortex core stability. Calculations show that: moving forward the loading of tip blade profile can reduce the pressure gradient;employing straight profile on the suction surface after passage throat can directly decrease the profile diffuse factor;and the redesigned blade by those two methods can obviously weaken the tip-leakage vortex, suppress the instability of vortex core and decrease the tip-leakage losses.

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