Numerical investigation of effect of outlet hub geometry on performance of large scale axial fan
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Numerical investigation of effect of outlet hub geometry on performance of large scale axial fan
Issue 5, (2014)
作者机构:
南京航空航天大学 能源与动力学院 江苏省航空动力系统重点实验室,南京,210016
作者简介:
基金信息:
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Published:2014
稿件说明:
移动端阅览
YIN Chao, HU Jun, TU Bao-feng, et al. Numerical investigation of effect of outlet hub geometry on performance of large scale axial fan[J]. 2014, (5).
DOI:
YIN Chao, HU Jun, TU Bao-feng, et al. Numerical investigation of effect of outlet hub geometry on performance of large scale axial fan[J]. 2014, (5).DOI:
Numerical investigation of effect of outlet hub geometry on performance of large scale axial fan
Four different outlet hub geometries of a large scale axial fan were designed and investigated. CFD methods were used to compare the fan characteristics and analyze the flow field structures in the blade tip and blade root. The results show that variation of outlet hub geometry has little effect on the fan's tip flow structure; there is a large separated flow in the blade root region which occupies 20% of blade height when the fan isn't provided with outlet hub
causing serious loss and decrease of efficiency; with the same blade tip clearance
the fan's efficiency increases when the outlet hub diffuser angle decreases; a matching straight or convergent hub could make the blade root separated vortex move backwards
reduce the separated area to 5% of blade height and increase at least 2 percentage points of the fan efficiency.