METHOD FOR DETERMINING THE ROTOR landing speed in gasdynamically plain bearings

摘要

method u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 landing speed rotor in u0433u0430u0437u043eu0434u0438u043du0430u043cu0438u0447u0435u0441u043au043eu043c u043fu043eu0434u0448u0438u043fu043du0438u043au0435 u0441u043au043eu043bu044cu0436u0435u043du0438u00a0, u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 is that it comes with u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 rotor bearing with the rotor load turn off drive u0434u0432u0438u0433u0430u0442u0435u043bu00a0 and u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 free braking of the rotor, the rotor speed and the time u0438u0437u043cu0435u0440u00a0u044eu0442 u0432u0440u0430u0449u0435u043du0438u00a0 u0442u0440u0435u043du0438u00a0 rotor in p u043eu0434u0448u0438u043fu043du0438u043au0435, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 ordersince the beginning u043du0430u0440u0430u0441u0442u0430u043du0438u00a0 moment u0442u0440u0435u043du0438u00a0 load decrease, and continue to u0438u0437u043cu0435u0440u0435u043du0438u00a0 before the start of the next u043du0430u0440u0430u0441u0442u0430u043du0438u00a0 moment u0442u0440u0435u043du0438u00a0 at a velocity u0432u0440u0430u0449u0435u043du0438u00a0 the rotor, in which the u043du0430u0447u0438u043du0430u0435u0442u0441u00a0 increased the u0442u0440u0435u043du0438u00a0, mistaken for the speed of the rotor u0434u043bu00a0 landing loads.