• Mayuresh Suresh Ingawale
• M. M. Khot
• S. D. Vispute
• Ohmkar Akhilesham

The air brake is a critical system of fighter aircraft which is operated by hydraulic system during landing to reduce the speed of aircraft. The model of air brake hydraulic system of fighter aircraft was built using AMESim software (advanced modeling environment for performing simulations of engineering systems). The different components of system such as swash plate axial piston pump, accumulator, bootstrap reservoir, and actuator are modeled and simulated individually and integrated in AMESim software. The model of air brake hydraulic system was simulated to analyze flow rates, pressure, and pressure drop and to determine actuation time of the air brake system. The theoretical calculations are also done for the same which gives the information about system pressure, flow rate and response time and compared with the results obtained from the simulation.

Air brake, Fighter aircraft, AMESim, Swash plate axial piston pump, Bootstrap reservoir

"Modeling and Simulation of Air Brake Hydraulic System of Fighter Aircraft using AMESim Software", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.316-323, June-2019, Available :http://www.jetir.org/papers/JETIR1906D94.pdf

"Modeling and Simulation of Air Brake Hydraulic System of Fighter Aircraft using AMESim Software", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp316-323, June-2019, Available at : http://www.jetir.org/papers/JETIR1906D94.pdf