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SEAL RING MOUNTING METHOD FOR TURBOCHARGER, AND TURBOCHARGER

机译:涡轮增压器的密封环安装方法以及涡轮增压器

摘要

It is intended to provide a seal ring mounting method for a turbocharger and a turbocharger with the seal ring, whereby the seal ring is less likely to be affected by other parts. An annular protrusion (12j) for restricting a position of a seal ring (16) in the radial direction is provided at a tip portion (12h) of an inner peripheral wall (12b) of a turbine housing (12), and the seal ring (16) is mounted between a side surface (36c) of a nozzle plate (36) and a first step portion (12k) of the tip portion (12h) of the inner peripheral wall (12b) so that the outer periphery of the seal ring (16) is restrained by the annular projection (12j).
机译:旨在提供一种用于涡轮增压器的密封环安装方法以及具有该密封环的涡轮增压器,由此该密封环不太可能受到其他部件的影响。在涡轮机壳体(12)的内周壁(12b)的顶端部(12h)设有用于限制密封环(16)的径向位置的环状的突起(12j),该密封环(16)被安装在喷嘴板(36)的侧面(36c)和内周壁(12b)的顶端部(12h)的第一台阶部(12k)之间,从而密封件的外周环形突起(12j)限制环(16)。

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