DocumentCode
2929157
Title
Simulation of Aircraft Fuel Thermal Management System Based on Simulink
Author
Liu Shuang ; Zhuang Damin ; Wanyan Xiaoru
Author_Institution
Sch. of Aeronaut. Sci. & Eng., BeiHang Univ., Beijing, China
fYear
2011
fDate
25-28 March 2011
Firstpage
1
Lastpage
4
Abstract
Aiming at the aircraft fuel system which adopts the technology of vapor cycle cooling system, and uses the fuel as a kind of effective cold source of condensers and other heat exchangers, this paper established the mathematical models of the fuel system and major components. On the basis of Simulink software platform, the simulation module of fuel system was established by developing the S-functions of the major components and the user-defined module library. According to the simulation module, the flow, temperature, pressure, and the import and export parameters of all the major components could be obtained in different given flight situations. The simulation module could also be used in making prediction and supervision of the thermal management and the parameters of each node of the aircraft fuel system, offering some reference for aircraft fuel system design which adopts the technology of vapor cycle cooling.
Keywords
aircraft; fuel systems; heat exchangers; mechanical engineering computing; thermal management (packaging); Simulink software; aircraft fuel thermal management system; condensers; heat exchangers; simulation module; vapor cycle cooling; Aerospace electronics; Aircraft; Atmospheric modeling; Fuel storage; Fuels; Heating; Mathematical model;
fLanguage
English
Publisher
ieee
Conference_Titel
Power and Energy Engineering Conference (APPEEC), 2011 Asia-Pacific
Conference_Location
Wuhan
ISSN
2157-4839
Print_ISBN
978-1-4244-6253-7
Type
conf
DOI
10.1109/APPEEC.2011.5748500
Filename
5748500
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