Study on Failure Mechanism of Steel Wire Wound Reinforced High-Pressure Hose

Article Preview

Abstract:

For steel wire wound reinforced high-pressure hose, the static load test under internal pressure and fatigue test under combined effect of internal pressure and periodic transverse load were carried out. Test results show that water seepage or leakage on the pressing steel sleeve or on hose body itself, and bulging on hose itself near steel joint would lead to performance failure, which can be regarded as the performance failure criterion for steel wire wound reinforced high-pressure hose.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 602-604)

Pages:

2219-2222

Citation:

Online since:

December 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Yang Yuwang, Zheng Ya, Qiu Guangshen, et al: Stress analysis and strength check of FRP/PVC composite pipe, Journal of Nanjing University of Science and Technology (Nature Science), 1995, Vol. 19(4), pp.381-384, (in Chinese).

Google Scholar

[2] Zhang Yue, Fan Xinmin, Kong Deren: Theoretical calculation of strength of laminated composite pipe, Journal of Ballis-tics, 2002, Vol. 14(1), pp.54-57, (in Chinese).

Google Scholar

[3] Zhou Jinghai, et al: Force Experiment and analysis of the UPVC underground water pipeline, Journal of Shenyang Jianzhu University, 2009, Vol. 25(6), pp.1069-1073, (in Chinese).

Google Scholar

[4] Wahab M. A., Alam M. S., Panga S. S.: Stress analysis of non-conventional composite pipes, Composite Structures, 2007, Vol. 79(1), pp.125-132.

DOI: 10.1016/j.compstruct.2005.11.054

Google Scholar

[5] Ren Zhimin, Ren Dongyun, Liu Kunlun, et al: FEA for a new type steel wire frame reinforced plastic composite pipe, China Plastics, 2002, Vol. 16(11), pp.40-43, (in Chinese).

Google Scholar

[6] Gargiulo C. A., Marchetti M. A., Rizzo A. A.: Prediction of failure envelopes of composite tubes subjected to biaxial loadings, ACTA Astronautica, 1996, Vol. 39(5), pp.355-368.

DOI: 10.1016/s0094-5765(96)00081-1

Google Scholar