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Rocket engines, acoustic channel COLLECTOR rocket engine and means of enhancing the efficiency of specific impulse rocket engine
Rocket engines, acoustic channel COLLECTOR rocket engine and means of enhancing the efficiency of specific impulse rocket engine
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机译:火箭发动机,声学通道COLLECTOR火箭发动机以及提高特定脉冲火箭发动机效率的方法
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摘要
1.the acoustic channels of the missile u0434u0432u0438u0433u0430u0442u0435u043bu00a0, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 because it contains a group of u043fu0440u043eu0445u043eu0434u00a0u0449u0438u0445 along the axis of acoustic channels formed around the axis u0442u00a0u0433u0438, a group of holes u0434u043bu00a0 u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e gas u0441u0432u00a0u0437u0430u043du043du044bu0445 with each of the u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 group of acoustic channels, and a circular manifold u0440u0430u0441u043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 constituted u0432u043eu043au0440 a. u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 axiswith the u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 circular collector u0440u0430u0441u043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u0441u0432u00a0u0437u0430u043d with each of the u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 group holes u0434u043bu00a0 u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e strip.;2. manifold for 1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 circular collector u0440u0430u0441u043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 contains a circular channel formed in the radially u0440u0430u0441u0445u043eu0434u00a0u0449u0435u0433u043eu0441u00a0 ring u043eu043bu043bu0435u043au0442u043eu0440u0430 acoustic channels.;3. manifold for 2, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0443u043fu043eu043cu00a0u043du0443u0442u043eu0435 radially u0440u0430u0441u0445u043eu0434u00a0u0449u0435u0435u0441u00a0 ring collector of acoustic channels supported on radius of cylindrical shell.;4. on u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 collector 3, so that u0443u043fu043eu043cu00a0u043du0443u0442u0430u00a0 group u0432u044bu0442u00a0u043du0443u0442u044bu0445 along the axis of acoustic channels formed on the inner surface of u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e u0446u0438u043bu0438u043du0434u0440u0438u0447u0435u0441u043a wow corps and served from u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 group u0432u044bu0442u00a0u043du0443u0442u044bu0445 along the axis of acoustic channels.;5. rocket engine injector containing a node u0441u0433u043eu0440u0430u043du0438u00a0 camera installed on the u0443u043fu043eu043cu00a0u043du0443u0442u043eu043c injector, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 because it contains manifold u0430u043au0443u0441u0442u0438u0447u0435u0441 u043au0438u0445 channels, the u0443u043fu043eu043cu00a0u043du0443u0442u043eu043c node u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 injector and collector of acoustic channels is connected to the u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 camera u0441u0433u043eu0440u0430u043du0438u00a0 and u0443u043fu043eu043cu00a0u043du0443u0442u0430u00a0 to u0430u043cu0435u0440u0430 u0441u0433u043eu0440u0430u043du0438u00a0 formed around the axis of u0442u00a0u0433u0438.;6. the on clause 5, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 sewer acoustic channels is installed on the outside perimeter u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e node u0438u043du0436u0435 spray head u043au0442u043eu0440u0430.;7. the on clause 5, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 sewer acoustic channels is fitted with a group of holes u0434u043bu00a0 u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e gas directed along the kama might u0441u0433u043eu0440u0430u043du0438u00a0.;8. the on clause 5, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 sewer acoustic signals formed by u0432u044bu0442u00a0u043du0443u0442u044bu0445 along the axis of acoustic channels located u0432u043eu043au0440 a. u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 axis u0442u00a0u0433u0438.;9. the engine u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 point 9, so that the axis of u0443u043fu043eu043cu00a0u043du0443u0442u044bu0445 u0432u044bu0442u00a0u043du0443u0442u044bu0445 along the axis of acoustic channels are directed along the wall of the camera u0441u0433u043eu0440u0430u043du0438u00a0.;10. the on clause 5, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 knot injector installed with the possibility of a supply of fuel to u043eu043au0438u0441u043bu0438u0442u0435u043bu00a0 and u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 cell u0441u0433u043eu0440u0430u043du0438u00a0.;11. the engine u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 clause 5, so that it further contains u043au043bu0430u043fu0430u043du043du0443u044e system of dual component of propellant, u0441u0432u00a0u0437u0430u043du043du0443u044e with u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e delivery system the possibility of synchronization u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e gas injecting gas, and fuel cell u043eu043au0438u0441u043bu0438u0442u0435u043bu00a0 u0443u043fu043eu043cu00a0u043du0443u0442u0443u044e u0441u0433u043eu0440u0430u043du0438u00a0.;12. the engine u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 p.11, so that it further contains a valve of the gas supply system u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e gas u0441u0432u00a0u0437u0430u043du043du044bu0439 with u0441u0438u043bu043eu0432u044b m u043fu043eu0440u0448u043du0435u043c valve valve chest system u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 dual component of propellant.;13. engine for p.u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 12, so that it further contains a subsidiary valve mounted with the possibility of u043fu0440u043eu0445u043eu0436u0434u0435u043du0438u00a0 through u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e stripwith the u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 subsidiary valve has an electrical u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 passing at the right moment u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e strip to u0443u043fu043eu043cu00a0u043d u0443u0442u043eu043cu0443 u0441u0438u043bu043eu0432u043eu043cu0443 acting on a piston valve and through the valve in the u043fu0440u0438u0432u0435u0434u0435u043du0438u00a0 twofold propellant u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 main stage valve chest two track system of propellant.;14. engine on p.13, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0443u043fu043eu043cu00a0u043du0443u0442u0430u00a0 system auxiliary valve installed with the possibility of u043fu0440u043eu0445u043eu0436u0434u0435u043du0438u00a0 in time u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e u0444u043eu0440u0441u0438u0440u0443u044eu0449 the gas manifold to u0443u043fu043eu043cu00a0u043du0443u0442u043eu043cu0443 acoustic channels through u0443u043fu043eu043cu00a0u043du0443u0442u044bu0439 valve of u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e strip.;15. method u043fu043eu0432u044bu0448u0435u043du0438u00a0 efficiency specific impulse rocket u0434u0432u0438u0433u0430u0442u0435u043bu00a0, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 u0438u043du0436u0435u043au0446u0438u044e u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e gas in the chamber through the manifold u0441u0433u043eu0440u0430u043du0438u00a0 ark u0441u0442u0438u0447u0435u0441u043au0438u0445 channels along the walls of the u0441u0433u043eu0440u0430u043du0438u00a0 formed around the axis of u0442u00a0u0433u0438.;16. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 p.15, however, further create vector flow, which u0444u043eu0440u0441u0438u0440u0443u044eu0449u0438u0439 gas directed along the wall of the camera u0441u0433u043eu0440u0430u043du0438u00a0, shape transition boundary layer u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e strip between the gas and wall u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e cameras u0441u0433u043eu0440u0430u043du0438u00a0.;17. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 p.15, so that as the u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e using helium gas.;18. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 p.15, so that as the u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e gas using hydrogen.;19. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 p.15, so that further u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 u0438u043du0436u0435u043au0446u0438u044e u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e strip in the acoustic channels at a pressure exceeding the pressure n wipe away the cameras u0441u0433u043eu0440u0430u043du0438u00a0.;20. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 p.15, however, further put u043au043bu0430u043fu0430u043du043du0443u044e dual component system rocket fuel to gas, and the valve of the u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e m sync u0438u043du0436u0435u043au0446u0438u044e u0444u043eu0440u0441u0438u0440u0443u044eu0449u0435u0433u043e gas u043eu043au0438u0441u043bu0438u0442u0435u043bu00a0 and fuel cell u0441u0433u043eu0440u0430u043du0438u00a0.
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