KR20040002526A - 터빈 - Google Patents

터빈 Download PDF

Info

Publication number
KR20040002526A
KR20040002526A KR1020030036019A KR20030036019A KR20040002526A KR 20040002526 A KR20040002526 A KR 20040002526A KR 1020030036019 A KR1020030036019 A KR 1020030036019A KR 20030036019 A KR20030036019 A KR 20030036019A KR 20040002526 A KR20040002526 A KR 20040002526A
Authority
KR
South Korea
Prior art keywords
turbine
vane
suction passage
trailing edge
turbine wheel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
KR1020030036019A
Other languages
English (en)
Korean (ko)
Inventor
샤프니콜라스
가렛트스티븐
Original Assignee
홀셋 엔지니어링 컴퍼니 리미티드
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 홀셋 엔지니어링 컴퍼니 리미티드 filed Critical 홀셋 엔지니어링 컴퍼니 리미티드
Publication of KR20040002526A publication Critical patent/KR20040002526A/ko
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/22—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
KR1020030036019A 2002-06-17 2003-06-04 터빈 Ceased KR20040002526A (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0213910.3A GB0213910D0 (en) 2002-06-17 2002-06-17 Turbine
GB0213910.3 2002-06-17

Publications (1)

Publication Number Publication Date
KR20040002526A true KR20040002526A (ko) 2004-01-07

Family

ID=9938744

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020030036019A Ceased KR20040002526A (ko) 2002-06-17 2003-06-04 터빈

Country Status (6)

Country Link
US (1) US6932565B2 (enExample)
EP (1) EP1375826B1 (enExample)
JP (1) JP2004019663A (enExample)
KR (1) KR20040002526A (enExample)
CN (1) CN1288333C (enExample)
GB (1) GB0213910D0 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101036591B1 (ko) * 2009-04-03 2011-05-24 김병섭 철근 커플러

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7150151B2 (en) * 2002-11-19 2006-12-19 Cummins Inc. Method of controlling the exhaust gas temperature for after-treatment systems on a diesel engine using a variable geometry turbine
US7207176B2 (en) 2002-11-19 2007-04-24 Cummins Inc. Method of controlling the exhaust gas temperature for after-treatment systems on a diesel engine using a variable geometry turbine
US7280950B2 (en) * 2004-01-22 2007-10-09 Electro-Motive Diesel, Inc. Locomotive diesel engine turbocharger and turbine stage constructed with turbine blade vibration suppression methodology
JP5140135B2 (ja) * 2004-05-06 2013-02-06 カミンズ インコーポレーテッド 可変幾何学的形態タービンを使用する内燃機関におけるあと処理システム用の排ガスの温度を決定する可変幾何学形態ターボ過給機及びシステム
DE102005027080A1 (de) * 2005-06-11 2006-12-14 Daimlerchrysler Ag Abgasturbine in einem Abgasturbolader
GB0521354D0 (en) * 2005-10-20 2005-11-30 Holset Engineering Co Variable geometry turbine
US20070175214A1 (en) * 2006-01-30 2007-08-02 Reisdorf Paul W Turbocharger having divided housing with nozzle vanes
GB0615495D0 (en) 2006-08-04 2006-09-13 Cummins Turbo Tech Ltd Variable geometry turbine
ITMI20061738A1 (it) * 2006-09-12 2008-03-13 Iveco Motorenforschung Ag Turbina a geometria variabile
CN101663466A (zh) * 2007-06-26 2010-03-03 博格华纳公司 可变几何形状的涡轮增压器
EP2077312A1 (en) 2007-12-17 2009-07-08 Nippon Oil Corporation Fuels for homogeneous charge compression ignition combustion engine
GB0805519D0 (en) * 2008-03-27 2008-04-30 Cummins Turbo Tech Ltd Variable geometry turbine
GB2462115A (en) * 2008-07-25 2010-01-27 Cummins Turbo Tech Ltd Variable geometry turbine
DE102010051359A1 (de) * 2010-11-13 2012-05-16 Daimler Ag Einsatzelement für eine Turbine eines Abgasturboladers, Abgasturbolader sowie Turbine für einen Abgasturbolader
JP5136701B2 (ja) * 2010-12-02 2013-02-06 トヨタ自動車株式会社 過給機付き内燃機関の制御装置
CN103946487B (zh) * 2011-11-30 2016-01-20 三菱重工业株式会社 径流式涡轮机
CN104471204B (zh) * 2012-07-27 2018-02-23 博格华纳公司 一种涡轮增压器和用于内燃发动机的涡轮增压器
DE102012108975A1 (de) * 2012-09-24 2014-03-27 Firma IHI Charging Systems International GmbH Verstellbarer Leitapparat für einen Abgasturbolader und Abgasturbolader
US9963974B2 (en) 2012-10-23 2018-05-08 United Technologies Corporation Reduction of equally spaced turbine nozzle vane excitation
GB2571356A (en) * 2018-02-27 2019-08-28 Cummins Ltd Variable geometry turbine
CN109779741B (zh) * 2019-01-23 2020-05-19 宁波天阁汽车零部件有限公司 一种车用涡轮增压器
JP7423557B2 (ja) * 2021-01-21 2024-01-29 三菱重工エンジン＆ターボチャージャ株式会社 可変容量タービンおよび過給機
US11732601B2 (en) 2021-12-06 2023-08-22 Borgwarner Inc. Variable turbine geometry assembly

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4292807A (en) * 1979-05-02 1981-10-06 United Technologies Corporation Variable geometry turbosupercharger system for internal combustion engine
US4318669A (en) * 1980-01-07 1982-03-09 The United States Of America As Represented By The Secretary Of The Air Force Vane configuration for fluid wake re-energization
DE3541508C1 (de) * 1985-11-23 1987-02-05 Kuehnle Kopp Kausch Ag Abgasturbolader
US4741666A (en) * 1985-12-23 1988-05-03 Ishikawajima-Harima Jukogyo Kabushiki Kaisha Variable displacement turbocharger
GB8829792D0 (en) * 1988-12-21 1989-07-05 Marconi Co Ltd Noise reduction method
JP3153409B2 (ja) * 1994-03-18 2001-04-09 株式会社日立製作所 遠心圧縮機の製作方法
AT405756B (de) * 1996-05-30 1999-11-25 Efg Turbinen Und Kraftwerksanl Leitschaufel für kaplanturbinen
GB2326198A (en) * 1997-06-10 1998-12-16 Holset Engineering Co Variable geometry turbine
AU2000267060A1 (en) * 2000-07-19 2002-01-30 Alliedsignal Turbo S.A. Sliding vane turbocharger with graduated vanes

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101036591B1 (ko) * 2009-04-03 2011-05-24 김병섭 철근 커플러

Also Published As

Publication number Publication date
CN1288333C (zh) 2006-12-06
EP1375826B1 (en) 2011-07-20
JP2004019663A (ja) 2004-01-22
GB0213910D0 (en) 2002-07-31
US20040101402A1 (en) 2004-05-27
EP1375826A1 (en) 2004-01-02
US6932565B2 (en) 2005-08-23
CN1469035A (zh) 2004-01-21

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PA0109 Patent application

Patent event code: PA01091R01D

Comment text: Patent Application

Patent event date: 20030604

PG1501 Laying open of application
A201 Request for examination
PA0201 Request for examination

Patent event code: PA02012R01D

Patent event date: 20080520

Comment text: Request for Examination of Application

Patent event code: PA02011R01I

Patent event date: 20030604

Comment text: Patent Application

E902 Notification of reason for refusal
PE0902 Notice of grounds for rejection

Comment text: Notification of reason for refusal

Patent event date: 20100511

Patent event code: PE09021S01D

E601 Decision to refuse application
PE0601 Decision on rejection of patent

Patent event date: 20100930

Comment text: Decision to Refuse Application

Patent event code: PE06012S01D

Patent event date: 20100511

Comment text: Notification of reason for refusal

Patent event code: PE06011S01I