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Turbine housing with a reinforcing ring partition wall opening

机译:涡轮机壳体,带加强圈分隔壁开口

摘要

A turbine housing segment (6) is disclosed. In one embodiment, a turbine housing segment (6) is disclosed that includes: a plurality of step segments (8), a plurality of reinforcement ring partitions (10) that separate the plurality of step segments (8), at least one of the plurality of reinforcement ring partitions (10) axially therethrough extending opening (11); and a substantially rounded suction opening (12) which is arranged flush with an inner surface (14) of one of the plurality of step segments (8).
机译:公开了一种涡轮机壳体段(6)。在一个实施例中,公开了一种涡轮机壳体段(6),其包括:多个阶梯段(8),将多个阶梯段(8)分开的多个加强环隔板(10),至少一个。轴向穿过其中的多个加强环隔板(10)延伸开口(11);基本上圆形的吸气口(12)与多个阶梯段(8)之一的内表面(14)齐平设置。

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