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Sealing systems TURBOCHARGER BEARING UNITS

机译:密封系统TURBOCHARGER BEARING UNITS

摘要

1.the turbocharger system seals bearing units, mainly from the compressor stage with u0442u0443u0440u0431u0438u043du043du043eu0435 and u043au043eu043cu043fu0440u0435u0441u0441u043eu0440u043du043eu0435 wheels, u0443u0441u0442u0430u043du043eu0432u043b u0435u043du043du044bu0435 separation on the end of the bearing units, a rotor, u0441u043eu0434u0435u0440u0436u0430u0449u0430u00a0 removable (- u043au043eu043bu044cu0446u0435u0434u0435u0440u0436u0430u0442u0435u043bu044c, not less than one u0440u0430u0437u0440u0435u0437u043du043eu0433u043e u043fu0440u0443u0436u0438u043du00a0u0449u0435 the u0443u043fu043bu043eu0442u043du0438u0442u0435u043bu044cu043du043eu0433u043e u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 rings, so that the cavity.u043eu0431u0440u0430u0437u043eu0432u0430u043du043du0430u00a0 separation between the back surface of the compressor working wheels and u0442u043eu0440u0446u0435u043c bearing units, connected through a radial slit. guests, an interior surface of the lid and u0442u043eu0440u0446u0435u043c shell bearing units with a closed annular u043cu0430u0441u043bu043eu0441u0431u043eu0440u043du0438u043au043eu043c located in peripheral part and the end surface of the bearing units.a u043fu043eu0434u043du0443u0442u0440u0435u043du0438u0435 toward the rotor and united in the bottom through u043eu0442u0432u0435u0440u0441u0442u0438u00a0 with u043fu0430u0442u0440u0443u0431u043au043eu043c oil drain, the closed circular u043cu0430u0441u043bu043eu0441u0431u043eu0440u043du0438u043au0430 u00a0 u0432u043bu00a0u044eu0442u0441u00a0 settlement and u0437u0430u0432u0438u0441u00a0u0442 from the gap.;2. the seals on u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 turbocharger bearing units 1, so that a closed ring u043cu0430u0441u043bu043eu0441u0431u043eu0440u043du0438u043a lies not only with the u043au043eu043cu043fu0440u0435u0441u0441u043e ra, but also by the turbine.;3. the turbocharger system seals for bearing units 1, u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0, however, that the optimal size of a closed circular u043cu0430u0441u043bu043eu0441u0431u043eu0440u043du0438u043au0430 u043du0430u0445u043eu0434u00a0u0442u0441u00a0 to follow consistent dependency:;d1 = (1,11,2) is dk; t = (56) b; l = (22.5); m = (44.5);where d1 is the outer diameter of the radial slit cavity bearing units;;is dk - diameter wheels (wheel turbine; compressor;;in the gap.;t is the width of the closed circular u043cu0430u0441u043bu043eu0441u0431u043eu0440u043du0438u043au0430;;l is the depth u043fu043eu0434u043du0443u0442u0440u0435u043du0438u00a0 closed circular u043cu0430u0441u043bu043eu0441u0431u043eu0440u043du0438u043au0430;;m is the height of a closed circular u043cu0430u0441u043bu043eu0441u0431u043eu0440u043du0438u043au0430
机译:1.涡轮增压器系统主要在压缩机级对轴承单元进行密封,其中 u0442 u0443 u0440 u0431 u0438 u043d u043d u043e u0435和 u043a u043e u043c u043f u0440 u0435 u0441 u0441 u043e u0440 u043d u043e u0435车轮, u0443 u0441 u0442 u0430 u043d u043e u0432 u043b u0435 u043d u043d u044b u0435轴承单元末端的分离,转子, u0441 u043e u0434 u0435 u0440 u0436 u0430 u0449 u0430 u00a0可移动(- u043a u043e u043b u044c u0446 u0435 u0434 u0435 u0435 u0440 u0436 u0430 u0444 u0434 u0435 u04340 u043b u044c,不少于一个 u0440 u0430 u0437 u0440 u0435 u0437 u043d u043e u0433 u043e u043f u0440 u0443 u0436 u0438 u043d u043d u00a0 u0449 u0435 u0443 u043f u043b u043e u0442 u043d u0438 u0442 u0435 u043b u044c u043d u043e u0433 u043e u043e u043e u0442 u043b u0438 u0447 u04447 u0430 u044e u0449 u0430 u04a u04a u00a0 u00a0振铃,以使空腔。 u043e u0431 u0440 u0430 u0437 u043e u0432 u0430 u043d u043d u0430 u00a0压缩机工作轮后表面之间的间隔和 u0442 u043e u0440 u0446 u0435 u043c轴承单元,它们通过径向缝隙连接。宾客,盖子的内表面和带有封闭环形 u043c u0430 u0441 u043b u043b u043e u0441 u0431 u043e u0440 u043d u043d u0435 u043a u043e u043c位于轴承单元的外围部分和端面。a u043f u043e u0434 u043d u0443 u0442 u0440 u0435 u043d u0438 u0435朝着转子并底部结合到 u043e u0442 u0432 u0435 u0440 u0441 u0442 u0438 u00a0和 u043f u0430 u0442 u0440 u0443 u0431 u043a u043e u043e排油口,闭合的圆形 u043c u0430 u0441 u043b u043e u0441 u0431 u043e u0440 u043d u0438 u043a u0430 u00a0 u0432 u043b u00a0 u044e u0442 u0441 u00a0结算和 u0437 u0430 u0432 u0438 u0441 u0442从差距开始; 2。 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0430 u00a0 u0441 u00a0涡轮增压器轴承单元1上的密封件,因此是封闭环 u043c u0430 u0441 u043b u043e u0441 u0431 u043e u0440 u043d u0438 u043a不仅位于 u043a u043e u043c u043c u043f u0440 u0435 u0441 u0441 u043e ra,而且还由涡轮机组成; 3。轴承单元1, u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0430 u00a0 u0441 u00a0的涡轮增压器系统密封件,但是,封闭圆形 u043c u0430 u0441的最佳尺寸 u043b u043e u0441 u0431 u043e u0440 u043d u0438 u043a u0430 u043d u0430 u0445 u043e u0434 u00a0 u0442 u0441 u00a0遵循一致的依赖性:; d1 =(1,11 ,2)是dk; t =(56)b; l =(22.5); m =(44.5);其中d1是径向狭缝腔轴承单元的外径;是dk-轮径(涡轮,压缩机;在间隙中).t是闭合圆形的宽度 u043c u0430 u0441 u043b u043e u0441 u0431 u043e u0440 u043d u0438 u043a u043a u0430 ;; l是深度 u043f u043e u0434 u043d u0443 u0442 u042 u0440 u0435 u043d u0438 u00a0闭合圆 u043c u0430 u0441 u043b u043e u0441 u0431 u043e u0440 u043d u0438 u043a u0430; m是闭合圆 u043c u0430 u0430 u0441 u043b u043e u0441的高度 u0431 u043e u0440 u043d u0438 u043a u0430

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