Aircraft Fuel Tank CATIA Model Pretreatment Method for Quality Property Calculation

Article Preview

Abstract:

According to the requirement of aircraft fuel quality property calculation, this paper studied pretreatment methods for tank CATIA model. Firstly, extract outside surfaces of wing skins, start and end wing ribs, front and back spars and then joint them to create a complete closed surface by additional repairing surfaces gap. Secondly, inside the closed surface, bool operation is utlized to remove actual bodies of fuel tank structures and internal accessories from the model of fuel tank. Direct accurate calculation of fuel quality property in CATIA environment is then achieved. Finally,simulation is carried out with an real aircraft fuel tank, comparison between simulation results and test data shows that relative error of pretreated fuel tank volume model is less than 1%, which satisfies engineering requirements.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

573-576

Citation:

Online since:

January 2015

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2015 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Xiao N. Research and development of the aircraft fuel measurement technology[J]. Aeronautical Science and Technology, 2003, (3): 31-34. (in Chinese).

Google Scholar

[2] Liu Z J, Yang F Z, Su S M. Research on aircraft fuel quality property calculations in the flight status[J]. Computer Simulation, 2013, 30(4): 72-76. (in Chinese).

Google Scholar

[3] Chang W. Calculation method research and simulation for aircraft fuel quality measurement[D]. Xi'an: Northwestern Polytechnical University, 2011. (in Chinese).

Google Scholar

[4] Su S M, Chang W, Wang H. Aircraft fuel tank volume characteristic database establishing and fuel quality measurement simulation[J]. Computer Measurement & Control, 2011, 19(9): 2091-2094. (in Chinese).

Google Scholar

[5] He M, Wang Z P, Han H Y. On computation of properties relating to quality of fuel needed in aircraft flight dynamics[J]. Journal of Northwestern Polytechnical University, 1996, 14(4): 617-621. (in Chinese).

Google Scholar

[6] Ohanian J O, III. Quality properties calculation and fuel analysis in the conceptual design of uninhabited air vehicles[D]. Virginia Polytechnic Institute and State University, (2003).

Google Scholar

[7] Jin Y L, Zhuang D M, Yang X. Modeling of airliner gasoline tank and modification of attitude error of sensor[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(2): 218-222. (in Chinese).

Google Scholar