Invention Grant
- Patent Title: Radial inflow turbine and turbocharger
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Application No.: US16967663Application Date: 2018-02-28
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Publication No.: US11339680B2Publication Date: 2022-05-24
- Inventor: Toyotaka Yoshida , Bipin Gupta , Yosuke Dammoto , Yoji Akiyama
- Applicant: MITSUBISHI HEAVY INDUSTRIES ENGINE & TURBOCHARGER, LTD.
- Applicant Address: JP Sagamihara
- Assignee: MITSUBISHI HEAVY INDUSTRIES ENGINE & TURBOCHARGER, LTD.
- Current Assignee: MITSUBISHI HEAVY INDUSTRIES ENGINE & TURBOCHARGER, LTD.
- Current Assignee Address: JP Sagamihara
- Agency: Birch, Stewart, Kolasch & Birch, LLP
- International Application: PCT/JP2018/007575 WO 20180228
- International Announcement: WO2019/167181 WO 20190906
- Main IPC: F01D17/16
- IPC: F01D17/16 ; F02B37/24 ; F01D9/02

Abstract:
A radial inflow turbine includes a scroll flow passage, a turbine wheel disposed radially inward of the scroll flow passage, a plurality of variable nozzle vanes disposed on a flow passage extending from the scroll flow passage toward the turbine wheel, at a radial position between the scroll flow passage and the turbine wheel, a nozzle mount rotatably supporting each of the plurality of variable nozzle vanes, a nozzle plate arranged to face the nozzle mount and forming the flow passage with the nozzle mount, and a swirl generating member disposed, radially outward of the plurality of variable nozzle vanes, on the nozzle plate in a height range which is smaller than that of a vane height of each of the plurality of variable nozzle vanes. A position of an end part of the swirl generating member on a side of the nozzle mount is farther away from the nozzle mount than a position of an end part of each of the plurality of variable nozzle vanes on the side of the nozzle mount in an axial direction.
Public/Granted literature
- US20210231027A1 RADIAL INFLOW TURBINE AND TURBOCHARGER Public/Granted day:2021-07-29
Information query
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