Design performance requirements and failure analysis of oxygen system on civil aircraft

Jian Wang

doi:10.1051/e3sconf/202123301076

All issues

Volume 233 (2021)

E3S Web Conf., 233 (2021) 01076

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		01076
Number of page(s)		4
Section		NESEE2020-New Energy Science and Environmental Engineering
DOI		https://doi.org/10.1051/e3sconf/202123301076
Published online		27 January 2021

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[1] “Aircraft Design Manual” General Editorial Committee. Aircraft Design Manual (Vol. 11). Interior of civil aircraft[M]. Beijing Aviation Industry Press, 2002. [Google Scholar]

[2] Junzhe Yao. A study on the monitoring of crew oxygen system leakage on Airbus A320 aircraft [J]. Aviation Maintenance and Engineering. 2018.79-82 [Google Scholar]

[3] Xu Tang. Safety design and assessment of oxygen systems for civil aviation [J]. Scientific and technical information. 2011 (22) [Google Scholar]

[4] Shcheglov. Heterogeneous equilibria in the rhenium-oxygen system.2006. [Google Scholar]

[5] W.H.Han, M.Miyake, T.Nagai, M.Maeda. Measurements of vapor pressure of Y and activity of Y-O alloy by multi-Knudsen cell mass.2009 1-2. [Google Scholar]