Measurements of three-dimensional flow field at exit of a turbine rotor passage in different tip clearances
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Measurements of three-dimensional flow field at exit of a turbine rotor passage in different tip clearances
Vol. 27, Issue 5, (2012)
作者机构:
1. 中国航空工业集团公司 燃气涡轮研究院, 四川 江油,621703
2. 南京航空航天大学 能源与动力学院,南京,210016
3. 北京航空航天大学 能源与动力工程学院,北京,100191
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基金信息:
DOI:
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Published:2012
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XIONG Bing, WAN Qian-jun, SHI Xiao-jiang, et al. Measurements of three-dimensional flow field at exit of a turbine rotor passage in different tip clearances[J]. 2012, 27(5).
DOI:
XIONG Bing, WAN Qian-jun, SHI Xiao-jiang, et al. Measurements of three-dimensional flow field at exit of a turbine rotor passage in different tip clearances[J]. 2012, 27(5).DOI:
Measurements of three-dimensional flow field at exit of a turbine rotor passage in different tip clearances
The time-resolved flow field downstream of a turbine rotor with different tip clearances was measured using a fast-response four-hole pressure probe.The results show that the flow is obviously periodic due to the rotor.It also indicates that the tip leakage flow has profound effects on the flow field.With bigger tip clearance
the leakage flow is relatively stronger and the secondary flow near the casing wall is weaker.When the tip gap is smaller
the secondary flow near the casing wall becomes stronger.The velocity in the leakage flow region is very low and the loss is high
which leads to substantial flow blockage.The flow under-turning due to the leakage flow is also clearly seen in the measurements.The static pressure in the leakage flow is higher than that in the main flow.The work done by the rotor with bigger tip clearance is lower than that with smaller tip clearance.
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Tip leakage flow and heat transfer characteristics with effect of trailing edge cutback on squealer tip
Numerical investigation of effect of forward sweep on tip clearance flows in highly loaded fan rotor
Modified blockage model of tip leakage flow and its validation
Combustor turbine interaction based on scale adaptive simulation
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CHENG Feng-na
CHANG Hai-ping
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TIAN Xing-jiang
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Related Institution
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
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