JP2012137068A5 - - Google Patents

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Publication number
JP2012137068A5
JP2012137068A5 JP2010291359A JP2010291359A JP2012137068A5 JP 2012137068 A5 JP2012137068 A5 JP 2012137068A5 JP 2010291359 A JP2010291359 A JP 2010291359A JP 2010291359 A JP2010291359 A JP 2010291359A JP 2012137068 A5 JP2012137068 A5 JP 2012137068A5
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JP
Japan
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JP2010291359A
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English (en)
Japanese (ja)
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JP2012137068A (ja
JP5433560B2 (ja
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Priority claimed from JP2010291359A external-priority patent/JP5433560B2/ja
Priority to JP2010291359A priority Critical patent/JP5433560B2/ja
Priority to CN201180052624.2A priority patent/CN103261622B/zh
Priority to US13/879,426 priority patent/US9328738B2/en
Priority to PCT/JP2011/079154 priority patent/WO2012090724A1/ja
Priority to EP11853195.3A priority patent/EP2617961B1/en
Publication of JP2012137068A publication Critical patent/JP2012137068A/ja
Publication of JP2012137068A5 publication Critical patent/JP2012137068A5/ja
Publication of JP5433560B2 publication Critical patent/JP5433560B2/ja
Application granted granted Critical
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2010291359A 2010-12-27 2010-12-27 タービンスクロール部構造 Expired - Fee Related JP5433560B2 (ja)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2010291359A JP5433560B2 (ja) 2010-12-27 2010-12-27 タービンスクロール部構造
EP11853195.3A EP2617961B1 (en) 2010-12-27 2011-12-16 Radial turbine
US13/879,426 US9328738B2 (en) 2010-12-27 2011-12-16 Turbine scroll part structure
PCT/JP2011/079154 WO2012090724A1 (ja) 2010-12-27 2011-12-16 タービンスクロール部構造
CN201180052624.2A CN103261622B (zh) 2010-12-27 2011-12-16 涡轮的涡旋部结构

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2010291359A JP5433560B2 (ja) 2010-12-27 2010-12-27 タービンスクロール部構造

Publications (3)

Publication Number Publication Date
JP2012137068A JP2012137068A (ja) 2012-07-19
JP2012137068A5 true JP2012137068A5 (OSRAM) 2013-05-16
JP5433560B2 JP5433560B2 (ja) 2014-03-05

Family

ID=46382837

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010291359A Expired - Fee Related JP5433560B2 (ja) 2010-12-27 2010-12-27 タービンスクロール部構造

Country Status (5)

Country Link
US (1) US9328738B2 (OSRAM)
EP (1) EP2617961B1 (OSRAM)
JP (1) JP5433560B2 (OSRAM)
CN (1) CN103261622B (OSRAM)
WO (1) WO2012090724A1 (OSRAM)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104870775B (zh) 2012-12-27 2017-07-28 三菱重工业株式会社 可变容量型排气涡轮增压器
WO2015076102A1 (ja) 2013-11-22 2015-05-28 株式会社Ihi 遠心圧縮機及び過給機
JP5870083B2 (ja) 2013-12-27 2016-02-24 三菱重工業株式会社 タービン
US10400617B2 (en) 2014-02-28 2019-09-03 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Sheet-metal turbine housing
CN105221334B (zh) * 2014-06-12 2016-12-14 山西华旗风能科技有限公司 一种集风装置
US10519850B2 (en) * 2014-11-04 2019-12-31 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Turbine housing and method of producing turbine housing
DE102015014900A1 (de) 2015-10-22 2017-04-27 GM Global Technology Operations LLC (n. d. Ges. d. Staates Delaware) Radialturbinengehäuse
CN108699959B (zh) * 2016-03-30 2020-10-02 三菱重工发动机和增压器株式会社 涡轮增压器
US10781704B2 (en) * 2016-12-28 2020-09-22 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Turbine and turbocharge
JP6947304B2 (ja) * 2018-06-29 2021-10-13 株式会社Ihi タービンおよび過給機
US11428108B2 (en) * 2019-02-25 2022-08-30 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Turbine housing and turbocharger
CN112443362B (zh) * 2019-08-29 2025-03-07 湖南天雁机械有限责任公司 减少涡舌激振力的涡轮箱结构
DE202021106090U1 (de) * 2021-11-08 2023-02-09 BorgWarner Inc. Turbinengehäuse für einen Abgasturbolader
US11851202B1 (en) 2022-06-23 2023-12-26 Pratt & Whitney Canada Corp. Aircraft engine, gas turbine intake therefore, and method of guiding exhaust gasses
US11891947B2 (en) 2022-06-23 2024-02-06 Pratt & Whitney Canada Corp. Aircraft engine, gas turbine intake therefore, and method of guiding exhaust gasses
US11821361B1 (en) 2022-07-06 2023-11-21 Pratt & Whitney Canada Corp. Gas turbine intake for aircraft engine and method of inspection thereof
US12188364B2 (en) 2022-07-06 2025-01-07 Pratt & Whitney Canada Corp. Damper segment for pressurized gas pipe of aircraft engine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4530640A (en) * 1982-09-29 1985-07-23 Roto-Master, Inc. Method and apparatus for wastegating turbocharged engine with divided exhaust system
JP3253978B2 (ja) 1990-12-10 2002-02-04 雅弘 井上 タービンスクロール
JP3586515B2 (ja) 1996-06-20 2004-11-10 三菱重工業株式会社 タービンスクロール
JPH10231706A (ja) * 1997-02-19 1998-09-02 Mitsubishi Heavy Ind Ltd タービンスクロール
FR2801072B1 (fr) * 1999-11-17 2002-11-08 Renault Turbocompresseur comportant des entrees de turbine alignees selon un plan radial
US6478553B1 (en) 2001-04-24 2002-11-12 General Motors Corporation High thrust turbocharger rotor with ball bearings
JP3534728B2 (ja) * 2001-10-19 2004-06-07 三菱重工業株式会社 ラジアルタービンのスクロール構造
US6742989B2 (en) 2001-10-19 2004-06-01 Mitsubishi Heavy Industries, Ltd. Structures of turbine scroll and blades
DE50312707D1 (de) 2003-03-19 2010-06-24 Abb Turbo Systems Ag Abgasturbinengehäuse
US20070089415A1 (en) * 2003-07-29 2007-04-26 Kiyohiro Shimokawa Turbocharger
JP4485334B2 (ja) * 2004-12-02 2010-06-23 トヨタ自動車株式会社 ターボチャージャのタービンハウジング
DE102007055507A1 (de) * 2007-11-21 2009-06-04 Georg Emanuel Koppenwallner Schräglippenspirale
US8266906B2 (en) * 2009-03-11 2012-09-18 GM Global Technology Operations LLC Asymmetric split-inlet turbine housing

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