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SEAL RING MOUNTING METHOD FOR TURBOCHARGER, AND TURBOCHARGER
SEAL RING MOUNTING METHOD FOR TURBOCHARGER, AND TURBOCHARGER
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机译:涡轮增压器的密封环安装方法以及涡轮增压器
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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).
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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。在顶端部分( 12 B> j I>)用于限制密封环( 16 B>)在径向上的位置。涡轮机壳体( 12 <的内周壁( 12 B> b I>)的 12 B> h I>) / B>),并在喷嘴板( 36 B> c I>)的侧面( 36 B> c I>)之间安装密封环( 16 B>)。 > 36 B>)和尖端部分( 12 B> h I)的第一步( 12 B> k I>) >)的内周壁( 12 B> b I>),从而使密封环( 16 B>)的外周受到环形凸起的约束( 12 B> j I>)。
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