Design of Integrative Testing System for Enclosures in Fuel System of Airplanes

Article Preview

Abstract:

In order to start performance testing and experimental research for enclosure of airplanes’ fuel systems, a type of integrative testing system is designed in this paper. This system can accomplish function and performance tests for enclosures in airplanes’ fuel system, and also can execute troubleshooting experiments.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

258-261

Citation:

Online since:

January 2015

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2015 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] ZHAO Dao-wen, LI Yue-dong, The design of synthesis test system for aircraft hydraulic accessories[J], MACHINE TOOL&HYDRAULICS, 2011(5): 37-38.

Google Scholar

[2] SONG Xiao-Jun, QING Hua, Study of Helicopter Fuel- system Components Test Bed[J], Hydraulics Pneumatics & Seals/No. 4. 2008: 83-84.

Google Scholar

[3] WANG Zhanyong, LIU Weifeng, The Design of Fuel Pump Test Desk for Fuel System of a Certain Airplane[J], MACHINE TOOL&HYDRAULICS, 2007(3): 14-16.

Google Scholar

[4] Juan F. Jimenez, Jose M. Giron-Sierra, C. Insaurralde, M. Seminario, A simulation of aircraft fuel management system, Simulation Modelling Practice and Theory, 2007, 15: 544-564.

DOI: 10.1016/j.simpat.2007.01.007

Google Scholar

[5] Raffi Babikian, Stephen P. Lukachko, Ian A. Waitz, The historical fuel efficiency characteristics of regional aircraft from technological, operational, and cost perspectives, Journal of Air Transport Management, vol. 8, issue. 2002, 8: 389-400.

DOI: 10.1016/s0969-6997(02)00020-0

Google Scholar

[6] Thomas H. Bradley, Blake A. Moffitt, Dimitri N. Mavris, David E. Parekh, Development and experimental characterization of a fuel cell powered aircraft, Journal of Power Sources, 2007, 171: 793-801.

DOI: 10.1016/j.jpowsour.2007.06.215

Google Scholar