METHOD adjusting the reverse thrust gas turbine engine on the run CHETYREHDVIGATELNOGO aircraft in use of reverse thrust four engines

摘要

method of u0440u0435u0433u0443u043bu0438u0440u043eu0432u0430u043du0438u00a0 feedback u0442u00a0u0433u0438 gas turbine engines for aircraft using the mileage u0447u0435u0442u044bu0440u0435u0445u0434u0432u0438u0433u0430u0442u0435u043bu044cu043du043eu0433u043e u0440u0435u0432u0435u0440u0441u0430 u0442u00a0u0433u0438 four u0434u0432u0438u0433u0430u0442u0435u043b her u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 so that, with a view to u0441u043du0438u0436u0435u043du0438u00a0 loads on the crew in the landing of aircraft engines and protection from u043fu043eu043fu0430u0434u0430u043du0438u00a0 u0440u0435u0432u0435u0440u0441u0438u0432u043d s of and foreign objects.;put on the surface of u043cu043eu0442u043eu0433u043eu043du0434u043eu043b external and internal engines are static u0434u0430u0432u043bu0435u043du0438u00a0;;compare the static u0434u0430u0432u043bu0435u043du0438u00a0 u043fu043eu043au0430u0437u0430u043du0438u00a0 receivers located on the surface of u043cu043eu0442u043eu0433u043eu043du0434u043eu043b external and internal engine, with u043fu043eu043au0430u0437u0430u043du0438u00a0u043cu0438 receiver u0432u043eu0437u0434u0443u0448 the main u0434u0430u0432u043bu0435u043du0438u00a0 (pa) in u0432u0440u0435u043cu00a0 distance plane using u0440u0435u0432u0435u0440u0441u0430 u0442u00a0u0433u0438;;in the absence of u0440u0430u0441u0441u043eu0433u043bu0430u0441u043eu0432u0430u043du0438u0439 between u043fu043eu043au0430u0437u0430u043du0438u00a0u043cu0438 static u0434u0430u0432u043bu0435u043du0438u00a0 receivers installed on the surface of u043cu043eu0442u043eu0433u043eu043du0434u043eu043b external and internal engine, and w the receiver u043eu043au0430u0437u0430u043du0438u00a0u043cu0438 air u0434u0430u0432u043bu0435u043du0438u00a0, a reverse u0442u00a0u0433u0438 engines u043eu0441u0442u0430u0432u043bu00a0u044eu0442 u043fu043eu0441u0442u043eu00a0u043du043du043eu0439;;in u043fu043eu00a0u0432u043bu0435u043du0438u0438 u0440u0430u0441u0441u043eu0433u043bu0430u0441u043eu0432u0430u043du0438u0439 between u043fu043eu043au0430u0437u0430u043du0438u00a0u043cu0438 static u0434u0430u0432u043bu0435u043du0438u00a0 receivers installed on the surface of u043cu043eu0442u043eu0433u043eu043du0434u043eu043b external and internal engine, and the u043fu043eu043au0430u0437u0430u043du0438u00a0u043cu0438's u0440u0430u0441u0441u043eu0433u043bu0430u0441u043eu0432u0430u043du0438u0439 between static u0434u0430u0432u043bu0435u043du0438u00a0 receivers installed on the surface of u043cu043eu0442u043eu0433u043eu043du0434u043eu043b external engines, with u043fu043eu043au0430u0437u0430u043du0438u00a0u043cu0438 receiver at u0437u0434u0443u0448u043du043eu0433u043e u0434u0430u0432u043bu0435u043du0438u00a0,u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 decrease the level of reverse u0442u00a0u0433u0438 internal engines until u0443u0441u0442u0440u0430u043du0438u0442u0441u00a0 u0440u0430u0441u0441u043eu0433u043bu0430u0441u043eu0432u0430u043du0438u0435 testimony by the number of static leni;where u0440u0441u0442.u0432u043du0435u0448u043d, u0440u0441u0442.u0432u043du0443u0442u0440 is the static u0434u0430u0432u043bu0435u043du0438u00a0 on u043cu043eu0442u043eu0433u043eu043du0434u043eu043bu0430u0445 external and internal engines;;u0440u0441u0442.u043fu0432u0434 is the static u0434u0430u0432u043bu0435u043du0438u00a0, u043fu043eu043bu0443u0447u0435u043du043du0430u00a0 from the air u0434u0430u0432u043bu0435u043du0438u00a0;;in u043fu043eu00a0u0432u043bu0435u043du0438u0438 u0440u0430u0441u0441u043eu0433u043bu0430u0441u043eu0432u0430u043du0438u0439 between u043fu043eu043au0430u0437u0430u043du0438u00a0u043cu0438 static u0434u0430u0432u043bu0435u043du0438u00a0 receivers installed on the surface of u043cu043eu0442u043eu0433u043eu043du0434u043eu043b external engines, and u043fu043eu043au0430u0437u0430u043du0438u00a0u043cu0438 ol u0438u0435u043cu043du0438u043au0430 air u0434u0430u0432u043bu0435u043du0438u00a0, as well as the lack of u0440u0430u0441u0441u043eu0433u043bu0430u0441u043eu0432u0430u043du0438u0439 between u043fu043eu043au0430u0437u0430u043du0438u00a0u043cu0438 static u0434u0430u0432u043bu0435u043du0438u00a0 receivers installed on the surface of u043cu043eu0442u043eu0433u043eu043du0434u043eu043b bh u0435u0448u043du0438u0445 and internal engineu043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 decrease the level of reverse u0442u00a0u0433u0438 external engines until the static blood pressure readings u0443u0441u0442u0440u0430u043du0438u0442u0441u00a0 u0440u0430u0441u0441u043eu0433u043bu0430u0441u043eu0432u0430u043du0438u0435 receivers and;comparison of static u0434u0430u0432u043bu0435u043du0438u00a0 receivers installed on the surface of u043cu043eu0442u043eu0433u043eu043du0434u043eu043b engines, and by the air u0434u0430u0432u043bu0435u043du0438u00a0 and raise e of the reverse u0442u00a0u0433u0438 aircraft engines for aircraft u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 u043fu0440u043eu0442u00a0u0436u0435u043du0438u0438 mileage up to u0432u044bu043au043bu044eu0447u0435u043du0438u00a0 u0440u0435u0432u0435u0440u0441u0430 u0442u00a0u0433u0438.