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TURBOCHARGER, TWO-STAGE TURBO SYSTEM, AND CONTROL METHOD FOR TWO-STAGE TURBO SYSTEM

机译:涡轮增压器,两阶段涡轮增压系统以及两阶段涡轮增压系统的控制方法

摘要

A turbocharger includes: at least two scroll passages, and a first range of the nozzle flow passage into which the exhaust gas flowing through the first scroll passage is introduced does not overlap with a second range of the nozzle flow passage into which the exhaust gas flowing through the second scroll passage is introduced, in a circumferential direction of the nozzle flow passage. The first scroll passage includes: a division wall disposed along a flow direction of the exhaust gas within a predetermined range in the first scroll passage, the division wall dividing the first scroll passage into a radially outer side scroll passage and a radially inner side scroll passage positioned on a radially inner side of the radially outer side scroll passage, and having a communication hole which brings the radially outer side scroll passage and the radially inner side scroll passage into communication; and a flow-rate control valve disposed on an upstream side of the division wall, for adjusting a flow rate of the exhaust gas flowing through the radially outer side scroll passage and the radially inner side scroll passage.
机译:一种涡轮增压器,包括:至少两个涡旋通道,并且被引入流过第一涡旋通道的排气的喷嘴流动通道的第一范围与排气流动的喷嘴流动通道的第二范围不重叠。在喷嘴流动通道的圆周方向上引入了穿过第二涡旋通道的通道。第一涡旋通道包括:在第一涡旋通道中沿排气的流动方向在预定范围内布置的分隔壁,该分隔壁将第一涡旋通道分隔成径向外侧涡旋通道和径向内侧涡旋通道。定位在径向外侧涡旋通道的径向内侧,并且具有连通孔,该连通孔使径向外侧涡旋通道和径向内侧涡旋通道连通。流量控制阀设置在分隔壁的上游侧,用于调节流过径向外侧涡旋通道和径向内侧涡旋通道的排气的流量。

著录项

  • 公开/公告号US2019078504A1

    专利类型

  • 公开/公告日2019-03-14

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY INDUSTRIES LTD.;

    申请/专利号US201716080269

  • 发明设计人 TOYOTAKA YOSHIDA;KUNIHIRO TOMIKAWA;

    申请日2017-03-03

  • 分类号F02B37/02;F02B37/18;F02B37/22;

  • 国家 US

  • 入库时间 2022-08-21 12:08:13

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