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Study on Preliminary Design of Fuel Transfer Jet Pump Using SIMULINK  

Kong Chang-Duk (조선대학교 항공조선공학부)
Park Jong-Ha (조선대학교 항공우주공학과)
Han Dong-Joo ((주)썬어에로시스 기술연구소)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.10, no.1, 2006 , pp. 38-43 More about this Journal
Abstract
In the present study, preliminary design and analysis for a jet pump, which is able to transfer fuel from the tank to the engine, were performed as an aerospace component technology development project. The jet pump is a core part, which is normally installed in the fuel tank, to supply the fuel from the tank to the engine feed pump, or to transfer the feed between tanks. In order to design preliminarily installed in the jet pump, equations for design were modelled using SIMULINK, and the design was carried out based on the simulation model.
Keywords
Jet Pump; Preliminary design; Fuel transfer; SIMULINK;
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  • Reference
1 Demil Y. Djafri, " T-91 Advanced Traniner Non-pressurised Fuel System", Msc Thesis, Cranfield Univ. U.K., 1992
2 Math Works, 1997, "SIMULINK: Dynamic System Simulation for MATLAB, Ver.2", The Math Works, Inc., USA
3 C.T., Lee, "Basic Military Trainer Fuel System", Msc Thesis, Cranfield Univ. U.K., 1985
4 공창덕 외 2인, "스마트 무인기 연료 시스템 설계에 관한 연구", 한국추진공학회지 제9권, 제2호, 2005, pp54-61
5 D.A. Phillips, "U-2000 Uninhabited Air Vehicle Fuel System", Msc Thesis, Cranfield Univ. U.K., 2001
6 ESDU 85032, "Ejectors and jet Pumps- Design and Performance for Incompressible Liquid flow", 1985
7 Demil Y. Djafri, " T-91 Advanced Traniner Non-pressurised Fuel System", Msc Thesis, Cranfield Univ. U.K., 1992