Abstract
Presented paper is focused on the performance analysis of turbofan engine with additional combustion chamber fueled by alternative fuel. Additional combustion chamber was situated between high pressure turbine and low pressure turbine. Such configuration is also know under the name inter turbine burner (ITB). As an alternative fuels burn in additional combustion chamber were selected cryogenics fuels: liquid hydrogen and liquid methane. The main combustion chamber was supplied by conventional aviation fuel - kerosene. Thermodynamic model of turbofan engine with ITB was implemented in MATLAB environment. The problem of modeling an additional combustion chamber was presented.Analysis was carried out for take-off conditions. Obtained results indicate that implementation of ITB exert a positive influence on engine performance result in thrust increase.
Publisher
Polish Scientific Society of Combustion Engines
Reference10 articles.
1. BUFFI, M.,CHIARAMONTI, D., VALERA-MEDINA, A. Strategies toward experimental assessments of new aviation renewable fuels and blends: the BIOREFLY project, Energy Procedia. 2017, 105, 433-438.
2. DAGGETT, D.L., HENDRICKS, R.C.,WALTHER, R.C., CORPORAN, E. Alternative fuels for use in commercial aircraft. 2007.
3. DAGGETT, D.L., HADALLER, O., HENDRICKS, R.C., WALTHER, R.C. Alternative fuels and their potential impact on aviation, NASA/TM–2006-214365, 2006.
4. EL-SAYED, A.F. Aircraft propulsion and gas turbine en-gines. CRC Press. 2017.
5. ANALYSIS OF CHOSEN FUELS INFLUENCE ON TURBOPROP ENGINE WORK PERFORMANCE
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献