METHOD OF ADJUSTING POWER CAPACITY OF AIRCRAFT ARRESTING GEAR, AND ARRESTING GEAR DESIGN

摘要

the invention u043eu0442u043du043eu0441u0438u0442u0441u00a0 to aviation technology, namely to the mobile u0430u044du0440u043eu0444u0438u043du0438u0448u0435u0440u0430u043c. purpose u0438u0437u043eu0431u0440u0435u0442u0435u043du0438u00a0 u00a0u0432u043bu00a0u0435u0442u0441u00a0 simplification of configuration u0430u044du0440u043eu0444u0438u043du0438u0448u0435u0440u0430 on energy consumption required value while improving the reliability and u0443u043fu0440u043eu0449u0435u043du0438 e system design u0442u043eu0440u043cu043eu0436u0435u043du0438u00a0 u0430u044du0440u043eu0444u0438u043du0438u0448u0435u0440u0430.in the method u0440u0435u0433u0443u043bu0438u0440u043eu0432u0430u043du0438u00a0 intensity u0430u044du0440u043eu0444u0438u043du0438u0448u0435u0438u0437u043eu0431u0440u0435u0442u0435u043du0438u0435 u043eu0442u043du043eu0441u0438u0442u0441u00a0 to aviation technology, namely to the mobile u0430u044du0440u043eu0444u0438u043du0438u0448u0435u0440u0430u043c. the closest no technical effect to the proposed u00a0u0432u043bu00a0u0435u0442u0441u00a0 u0430u044du0440u043eu0444u0438u043du0438u0448u0435u0440 with u0433u0438u0434u0440u043eu0434u0438u043du0430u043cu0438u0447u0435u0441u043au0438u043c brake (german patent no. 1290824. in 64 f 27 / 01, 1969).regulation of u0433u0438u0434u0440u043eu0442u043eu0440u043cu043eu0437u0430 u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u0435u0442u0441u00a0 flap mounted between the wheels u0433u0438u0434u0440u043eu0442u043eu0440u043cu043eu0437u0430 and ra, u0437u0430u043au043bu044eu0447u0430u044eu0449u0435u043cu0441u00a0 in u043du0430u043cu043eu0442u043au0435 tape receiver on the drum and a brake u0443u0441u0438u043bu0438u00a0 in u0440u0430u0437u043cu043eu0442u043au0435 ribbon with a drum for receiving the next aircraft impose its weight and the u0441u043au043eu0440u043eu0441 are youthe established parameters u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 aircraft initial radius of winding tape and rotate the drum u0430u044du0440u043eu0444u0438u043du0438u0448u0435u0440u0430 to u0434u043eu0441u0442u0438u0436u0435u043du0438u00a0 u0437u043du0430u0447u0435u043d u0438u00a0 primary winding radius. in u0430u044du0440u043eu0444u0438u043du0438u0448u0435u0440u0435 containing u0433u0438u0434u0440u043eu0434u0438u043du0430u043cu0438u0447u0435u0441u043au0438u0439 brake rotor 1, which is connected with a winding drum 3 of the tape 4, the drum has two stationary rollers 6. and 8 and a movable roller 7 between them.tape 4 and through the rollers 6 to 8 with the formation of loops, and the movable roller 7 u0441u043eu0435u0434u0438u043fu043du0435u043d with u043fu0435u0440u0435u043cu0435u0449u0430u044eu0449u0438u043c his drive in the form of u0433u0438u0434u0440u043eu0446u0438u043bu0438u043du0434u0440u0430 9 so that, in the setting the initial radius of belt webbing u043bu0435u043du0442u044cu0433 between the drum 3 and the reception device u0432u044bu0431u0438u0440u0430u0435u0442u0441u00a0 by u043eu0431u0440u0430u0437u043eu0432u0430u043du0438u00a0 loop tape of reel 7.1).sl with u043fu0440u043eu0438u0437u0432u043eu0434u0438u0442u044cu0441u00a0 as the u0442u043eu0440u043cu043eu0436u0435u043du0438u00a0, and before boarding the aircraft (la). a disadvantage of this technical u0440u0435u0448u0435u043du0438u00a0 u00a0u0432u043bu00a0u0435u0442u0441u00a0 what u044du043du0435u0440u0433u0438u00a0, u043fu043eu0433u043bu043eu0449u0430u0435u043cu0430u00a0 u0433u0438u0434u0440u043eu0442u043eu0440u043cu043eu0437u043eu043c significantly depends on the frequency of u0432u0440u0430u0449u0435u043du0438u00a0 rotor u0433u0438u0434u0440u043eu0442u043eu0440u043cu043eu0437u0430, kotor u00a0 u043eu043fu0440u0435u0434u0435u043bu00a0u0435u0442u0441u00a0 landing at la. the frequency of u0432u0440u0430u0449u0435u043du0438u00a0 rotor and opening of the louvers u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 quantity of energy absorbed.the minimum number of hours | sl on the ok