Influence on aerodynamic performance of a highly loaded two-stage fan with variable inlet guide vane

被引:0
作者
机构
[1] School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing
[2] China Gas Turbine Establishment, Aviation Industry Corporation of China, Chengdu
来源
| 1600年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 29期
关键词
Aerodynamic performance; Highly loaded; Prewhirl angle; Two-stage fan; Variable inlet guide vane;
D O I
10.13224/j.cnki.jasp.2014.12.026
中图分类号
学科分类号
摘要
In order to improve the stall margin and decrease the rotor attack angle of a highly loaded two-stage fan at off-design speed, different forms of variable inlet guide vane(VIGV) and traditional adjustable inlet guide vane were simulated, and the aerodynamic performance and internal flow field of highly loaded two-stage fan were analyzed. The numerical simulation results show that: at the 80% design speed, the highly loaded two-stage fan's adiabatic efficiency increases obviously with the increase of the VIGV's positive prewhirl, and the adiabatic efficiency increases 3.5% with prewhirl angle of 30 degrees; although traditional adjustable inlet guide vane has a better effect on the expanding stability, the loss is biggest when it needs a large prewhirl angle; the slot form, the slot position and the solidity of VIGV have a considerable influence on aerodynamic performance, with the design depending on the particular working conditions of the highly loaded two-stage fan. ©, 2014, BUAA Press. All right reserved.
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页码:2973 / 2979
页数:6
相关论文
共 19 条
[1]  
Liu D., The development and proposals of aeroengine technology, Engineering Science, 1, 2, pp. 24-29, (1999)
[2]  
Creason T.L., Baghdadi S., Design and test of a low aspect ratio fan stage, (1988)
[3]  
Hasegawa H., Development of highly loaded fan with tandem cascade, (2003)
[4]  
Hu G., Zhou Y., Chen B., Et al., Design and test for single stage transonic fan with high speed, high load, Journal of Engineering Thermophysics, 22, 1, pp. 40-43, (2001)
[5]  
Jin H., Jin D., Gui X., Aerodynamic design and numerical simulation of a highly loaded transonic two-stage fan, Journal of Aerospace Power, 26, 2, pp. 272-280, (2011)
[6]  
Liu Z., Zhao F., Hui Z., Et al., An experimental study on a new type of variable-geometry guide vanes, Journal of Engineering for Thermal Energy and Power, 5, 1, pp. 1-4, (1990)
[7]  
Liu Z., Zhao F., Mu S., Et al., An experimental study of variable camper cascades, Journal of Engineering for Thermal Energy and Power, 6, 3, pp. 113-121, (1991)
[8]  
Seroy G.K., Kavanagh P., Considerations in the design of variable geometry blading for axial compressor stages, (1968)
[9]  
Bobula G.A., Soeder R.H., Burkarolt L.A., Effect of a part-span variable inlet guide vane on the performance of a high-bypass turbofan engine, (1981)
[10]  
Woollett R.R., Aerodynamic performance of a fan stage utilizing variable inlet guide vanes for thrust modulation, AIAA/SAE/ASME 19th Joint Propulsion Conference, (1983)