• DHIRAJ DHANAJI PATIL
• P. D. Maskar,
• Amit Kumar Soni

Eastern way of developing aircraft mainly focuses on mechanical based actuation fuel system components and auxiliary units. Fuel system uses pressurized fuel for its working. To model this type of system AMESim software (Advanced Modeling Environment for performing Simulations of engineering systems) is used as a basic platform. Tank volumetric design and data file generation is carried out using CATIA software for simulation requirement. Using available libraries mechanical components are created. Command and Control system which manages fuel flow within tanks and to the engine is integrated to the main fuel system. Jet Transducer is a controlling mechanical element modeled using signals and state chart also Hydro booster pump is created using thermal hydraulic library. The model of fuel system was simulated and analyzed for flow rates, tank pressure and % MAC variation with respect to time and fuel consumption. Ground testing results are used to compare results of simulation.

AMESim, Data File, Jet Transducer, Hydro Booster Pump, MAC, Modeling

"Modeling and Simulation of Command and Control System to Execute the Fuel Sequencing for Fighter Aircraft using AMESim", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.690-697, June-2019, Available :http://www.jetir.org/papers/JETIR1906G07.pdf

"Modeling and Simulation of Command and Control System to Execute the Fuel Sequencing for Fighter Aircraft using AMESim", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp690-697, June-2019, Available at : http://www.jetir.org/papers/JETIR1906G07.pdf