The impact of the simple orifice schemes of the buffer device in boom refuelling system in the transient pressure of the pipeline

Zhangzhi Dong; Xiaogang Li; Yanyan Hou; Bin Li; Yujuan He

doi:10.1051/e3sconf/202123304015

All issues

Volume 233 (2021)

E3S Web Conf., 233 (2021) 04015

References

Open Access

Issue		E3S Web Conf. Volume 233, 2021 2020 2^nd International Academic Exchange Conference on Science and Technology Innovation (IAECST 2020)


Article Number		04015
Number of page(s)		5
Section		MEA2020-Mechanical Engineering and Automation
DOI		https://doi.org/10.1051/e3sconf/202123304015
Published online		27 January 2021

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[1] Parks, S. E. , and M. E. Franke et al.,. “Transient flow analysis of an aircraft refueling system”, J. Aircraft., vol. 20, no. 12, pp. 1033-1036, 1971. [CrossRef] [Google Scholar]

[2] H. W. Ng, and F. L. Tan, “Simulation of fuel behaviour during aircraft in-flight refueling”, Aircr. Eng. Aerosp. Tec., vol. 81, no. 2, pp. 99-105, 2009. [CrossRef] [Google Scholar]

[3] R.-X. Zhou, et al., “Aircraft Pressure Refueling Pipeline Dynamic Pressure Control Technology”, Journal of Air Force Engineering Universityꞏ(Natural Science Edition), vol. 5, pp. 1-3, 2003. [Google Scholar]

[4] J.-W. Tian, “Analysis of the development of China’s aerial tanker”, Tank and armored vehicles, vol. 20, pp. 20-24, 2016. doi:10.19486/j.cnki.11-1936/tj.2016.20.008. [Google Scholar]

[5] X.-D. Kong, X.-X. Zhu, L.-X. Quan et al., “Simulation study of pressure shock absorption by proportional valve-controlled accumulator”, Machine tools and hydraulics, vol. 11, pp. 131-134+81, 2018. [Google Scholar]