Effects of Ice Thickness on the Aerodynamic Characteristics of Crescent Shape Iced Conductors

Article Preview

Abstract:

Aerodynamic characteristics of iced conductors were investigated by the wind tunnel test. Under the homogeneous turbulence of 5% intensity, aerodynamic force coefficients of single and bundled conductors were obtained at wind angles of 0°~180°. The variation patterns of aerodynamic forces on the iced conductors with respect to wind angels of attack were systematically studied for the ice thickness of 0.25, 0.5, 0.75 and 1 times of the conductor diameter. The difference of aerodynamic force characteristics for single and bundled conductors were identified and discussed. Based on the Den Hartog and Nigol’s mechanisms of galloping, the wind angle ranges sensitive to galloping were analyzed. The results show that lift and torsion force coefficients reach peak values at wind angles of 15°~20°. For bundled conductors, lift force curve is approximately agreed with the curve of single conductor. Drag force coefficients were smaller than these of single conductor at some wind angles. There are noticeably differences of torsion coefficients existed between bundled conductors and single conductor. According to two classical galloping mechanisms, wind angles of 15°~30°are critical for the galloping of iced conductors with crescent shapes.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

2696-2703

Citation:

Online since:

May 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Morishita,S., et al., Galloping phenomena of large bundled conductors experimental results of the field test lines, International Conference on Large High Voltage Electric Systems, SC22-04,(1984)

Google Scholar

[2] Kikuchi,T., et al.: Journal of the Japanese Society of Snow and Ice, Vol.68(5) ( 2006), pp.457-466

Google Scholar

[3] Yukino,T., et al., Experiment of snow accretion and geometrical analysis of the shape, 8th International Workshop on Atmospheric Icing of Structures,(1998), pp.95-99

Google Scholar

[4] CIGRE, State of the art of conductor galloping, CIGRE Technical Brochure,No,322,TF B2.11.O6. (2007)

Google Scholar

[5] Xin Wang, Wenjuan Lou, Guohui Shen, et al.: Acta aerodynamic sinica. Vol.29(5) (2011), pp.573-579 (in Chinese)

Google Scholar

[6] Ming Gu, Wenyong Ma, Yong Quan, et al.: Journal of Tongji University (Natural Science). Vol. 37(10) (2009),pp.1328-1332. (in Chinese)

Google Scholar

[7] Yi Lv, Wenjuan Lou, Zhenmao Sun, et al.: Journal of Zhejiang University (Engineering Science). Vol.44(1) (2010), pp.174-179

Google Scholar

[8] DenHartog J P.Transmission line vibration due to sleet. AIEE Transaction. 1932, part 4:1074-1086

Google Scholar

[9] NIGOL O, BUCHAN P G.: IEEE Transactions on Power Apparatus and Systems, Vol.100(2) (1981), pp.708-720

DOI: 10.1109/tpas.1981.316922

Google Scholar