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Jet Engine Fuel System Integration in Aircraft Environment - Methodology for Pressure Surge Simulation through Model-Based System Engineering
Journal Article
2014-01-2135
ISSN: 1946-3855, e-ISSN: 1946-3901
Sector:
Citation:
Hutchison, M., Lenoble, G., Badiali, U., Sommerer, Y. et al., "Jet Engine Fuel System Integration in Aircraft Environment - Methodology for Pressure Surge Simulation through Model-Based System Engineering," SAE Int. J. Aerosp. 7(1):74-89, 2014, https://doi.org/10.4271/2014-01-2135.
Language:
English
Abstract:
An Airbus methodology for the assessment of accurate fuel pressure surge at early program stages in the complete aircraft and engine environment based on joint collaboration with LMS Engineering is presented. The aim is to comfort the prediction of the fuel pressure spike generated by an engine shutdown in order to avoid late airframe fuel system redesign and secure the aircraft entry-into-service.
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