Hypersonic ramjet engine (scramjet) AND METHOD OF BURNING

摘要

1. u0433u0438u043fu0435u0440u0437u0432u0443u043au043eu0432u043eu0439 u043fu0440u00a0u043cu043eu0442u043eu0447u043du044bu0439 jet engine (u0433u043fu0432u0440u0434) containing the nasal part of the nozzle, air intake, fuel cell u0441u0433u043eu0440u0430u043du0438u00a0 and nozzle, differing u0438u0439u0441u00a0, u0442u043eu043fu043bu0438u0432u043du0430u00a0 fuel injector is located in a part of the u0434u0432u0438u0433u0430u0442u0435u043bu00a0 before a shaker on its axis and is connected with a shaker pylons.;2. the way the u0433u043eu0440u0435u043du0438u00a0 in u0433u0438u043fu0435u0440u0437u0432u0443u043au043eu0432u043eu043c u043fu0440u00a0u043cu043eu0442u043eu0447u043du043eu043c air jet engine (u0433u043fu0432u0440u0434), u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 in a fuel cell u0441u0433u043eu0440u0430u043du0438u00a0, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 order the fuel supply to a shaker that u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 zone formed between the fuel nozzle, pylons and a shaker.;3. the engine 1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0440u0430u0441u0441u0442u043eu00a0u043du0438u0435 between the fuel nozzle and the ratio of a shaker;l = kd.;where l is u0440u0430u0441u0441u0442u043eu00a0u043du0438u0435 between the fuel nozzle and a shaker.;the rate of u043fu043eu0434u043eu0431u0438u00a0;;d is the diameter of the air.;4. the engine 1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, running and management u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 office air fuel from the fuel nozzle with the help of the the computer.