DE60030894D1 - Turbokompressor mit axial verschiebbaren leitschaufeln wobei die geometrie in längsrichtung unterschiedlich ist - Google Patents

Turbokompressor mit axial verschiebbaren leitschaufeln wobei die geometrie in längsrichtung unterschiedlich ist

Info

Publication number
DE60030894D1
DE60030894D1 DE60030894T DE60030894T DE60030894D1 DE 60030894 D1 DE60030894 D1 DE 60030894D1 DE 60030894 T DE60030894 T DE 60030894T DE 60030894 T DE60030894 T DE 60030894T DE 60030894 D1 DE60030894 D1 DE 60030894D1
Authority
DE
Germany
Prior art keywords
turbokompressor
geometry
length direction
movable guide
axial movable
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.)
Expired - Lifetime
Application number
DE60030894T
Other languages
English (en)
Other versions
DE60030894T2 (de
Inventor
Alain Rene Lombard
Jean-Luc Hubert Perrin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Garrett Motion France SAS
Original Assignee
Honeywell Garrett SA
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 Honeywell Garrett SA filed Critical Honeywell Garrett SA
Publication of DE60030894D1 publication Critical patent/DE60030894D1/de
Application granted granted Critical
Publication of DE60030894T2 publication Critical patent/DE60030894T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F01D17/143—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path the shiftable member being a wall, or part thereof of a radial diffuser
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
DE60030894T 2000-07-19 2000-07-19 Turbokompressor mit axial verschiebbaren schaufeln wobei die geometrie in längsrichtung unterschiedlich ist Expired - Lifetime DE60030894T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/FR2000/002069 WO2002006636A1 (fr) 2000-07-19 2000-07-19 Turbocompresseur a ailettes coulissantes avec ailettes graduees

Publications (2)

Publication Number Publication Date
DE60030894D1 true DE60030894D1 (de) 2006-11-02
DE60030894T2 DE60030894T2 (de) 2007-09-06

Family

ID=8847165

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60030894T Expired - Lifetime DE60030894T2 (de) 2000-07-19 2000-07-19 Turbokompressor mit axial verschiebbaren schaufeln wobei die geometrie in längsrichtung unterschiedlich ist

Country Status (8)

Country Link
US (1) US7097432B1 (de)
EP (1) EP1301689B1 (de)
JP (1) JP2004504524A (de)
KR (1) KR100643093B1 (de)
CN (1) CN1289791C (de)
AU (1) AU2000267060A1 (de)
DE (1) DE60030894T2 (de)
WO (1) WO2002006636A1 (de)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6652224B2 (en) 2002-04-08 2003-11-25 Holset Engineering Company Ltd. Variable geometry turbine
GB0213910D0 (en) 2002-06-17 2002-07-31 Holset Engineering Co Turbine
EP1561007B1 (de) * 2002-11-15 2006-10-11 Honeywell International, Inc. Variable düse für turbolader
US8608433B2 (en) * 2003-02-19 2013-12-17 Honeywell International, Inc. Turbine having variable throat
US7458764B2 (en) * 2003-02-19 2008-12-02 Honeywell International, Inc. Nozzle device for a turbocharger and associated control method
US8197194B2 (en) 2004-05-03 2012-06-12 Honeywell International, Inc. Turbine of a turbocharger
WO2005106212A1 (en) * 2004-05-03 2005-11-10 Honeywell International Inc. Center housing of a turbine for a turbocharger and method of manufacturing the same
US8047772B2 (en) * 2005-03-30 2011-11-01 Honeywell International Inc. Variable geometry turbine for a turbocharger and method of controlling the turbine
JP4468286B2 (ja) * 2005-10-21 2010-05-26 三菱重工業株式会社 排気ターボ式過給機
US8197195B2 (en) 2005-11-16 2012-06-12 Honeywell International Inc. Turbocharger with stepped two-stage vane nozzle
US7338254B2 (en) * 2005-11-29 2008-03-04 Honeywell International, Inc. Turbocharger with sliding piston assembly
EP1816317B1 (de) * 2006-02-02 2013-06-12 IHI Corporation Turbolader mit variabler Geometrie
WO2007148390A1 (ja) * 2006-06-21 2007-12-27 Ihi Corporation 回転機械の軸受構造、回転機械、軸受構造の製造方法、並びに回転機械の製造方法
JP5238711B2 (ja) * 2006-11-01 2013-07-17 ボーグワーナー インコーポレーテッド タービン防熱材組立体
US7980816B2 (en) * 2007-08-27 2011-07-19 Honeywell International Inc. Retainer for a turbocharger
GB0805519D0 (en) * 2008-03-27 2008-04-30 Cummins Turbo Tech Ltd Variable geometry turbine
DE102008023552B4 (de) * 2008-05-14 2018-12-20 BMTS Technology GmbH & Co. KG Abgasturbolader für ein Kraftfahrzeug
GB2461720B (en) 2008-07-10 2012-09-05 Cummins Turbo Tech Ltd A variable geometry turbine
GB2462115A (en) * 2008-07-25 2010-01-27 Cummins Turbo Tech Ltd Variable geometry turbine
KR101012085B1 (ko) * 2009-03-05 2011-02-07 방규열 부류식 수력발전장치
GB2468871B (en) * 2009-03-25 2015-03-18 Cummins Turbo Tech Ltd Turbocharger
DE102009053238B4 (de) * 2009-11-13 2012-06-21 Continental Automotive Gmbh Turboladergehäuse mit einer Dichtungseinrichtung
JP5473762B2 (ja) * 2010-04-30 2014-04-16 三菱重工業株式会社 可変容量タービンおよびこれを備えた可変容量ターボチャージャ
KR101924920B1 (ko) * 2011-06-10 2018-12-04 보르그워너 인코퍼레이티드 복류식 터빈 하우징 터보차저
DE102011109643A1 (de) 2011-08-05 2013-02-07 Daimler Ag Turbine für einen Abgasturbolader
JP5409741B2 (ja) 2011-09-28 2014-02-05 三菱重工業株式会社 可変ノズル機構の開度規制構造および可変容量型ターボチャージャ
DE102011120555A1 (de) 2011-12-08 2013-06-13 Daimler Ag Leitgitter für eine Turbine eines Abgasturboladers sowie Turbine für einen Abgasturbolader
DE102011120553A1 (de) 2011-12-08 2013-06-13 Daimler Ag Turbine für einen Abgasturbolader
US9950382B2 (en) * 2012-03-23 2018-04-24 Pratt & Whitney Canada Corp. Method for a fabricated heat shield with rails and studs mounted on the cold side of a combustor heat shield
CN104956045A (zh) * 2013-02-19 2015-09-30 博格华纳公司 具有轴流式转动叶片的涡轮增压器内部涡轮机隔热屏
GB2555872A (en) 2016-11-15 2018-05-16 Cummins Ltd Vane arrangement for a turbo-machine
GB2574195B (en) * 2018-05-15 2022-06-08 Cummins Ltd Vane and shroud arrangements for a turbo-machine
CN110496556A (zh) * 2019-09-16 2019-11-26 中煤科工清洁能源股份有限公司 一种给料系统
US11686210B2 (en) * 2021-03-24 2023-06-27 General Electric Company Component assembly for variable airfoil systems

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2914300A (en) * 1955-12-22 1959-11-24 Gen Electric Nozzle vane support for turbines
US3749513A (en) 1970-09-22 1973-07-31 Eaton Corp Fluid turbomotor
US3836282A (en) * 1973-03-28 1974-09-17 United Aircraft Corp Stator vane support and construction thereof
EP0095853B1 (de) * 1982-05-28 1988-08-03 Holset Engineering Company Limited Turbine mit verstellbarem Zufuhrquerschnitt
US4726744A (en) * 1985-10-24 1988-02-23 Household Manufacturing, Inc. Tubocharger with variable vane
US5214920A (en) 1990-11-27 1993-06-01 Leavesley Malcolm G Turbocharger apparatus
DE4232400C1 (de) * 1992-03-14 1993-08-19 Mercedes-Benz Aktiengesellschaft, 7000 Stuttgart, De
DE4215301A1 (de) 1992-05-09 1993-11-11 Mak Maschinenbau Krupp Abgasturbolader mit einer Radialturbine
DE69308377T2 (de) * 1992-05-21 1997-06-19 Alliedsignal Ltd Regelbarer Turbolader
DE4218229C1 (en) * 1992-06-03 1993-03-04 Man B & W Diesel Ag, 8900 Augsburg, De Turbocharger with radial flow through impeller - has blade retaining recesses, into which blades are insertable after axial shift of adjuster
US5231831A (en) 1992-07-28 1993-08-03 Leavesley Malcolm G Turbocharger apparatus
US5248240A (en) * 1993-02-08 1993-09-28 General Electric Company Turbine stator vane assembly
US5947681A (en) 1997-03-17 1999-09-07 Alliedsignal Inc. Pressure balanced dual axle variable nozzle turbocharger
MXPA02006864A (es) * 2000-01-14 2002-10-23 Alliedsignal Turbo S A Turbo compresor con aletas deslizantes con superficies aerodinamicas y pantalla termica combinadas, y dispositivo de accionamiento axial desacoplado.

Also Published As

Publication number Publication date
KR20030029785A (ko) 2003-04-16
EP1301689A1 (de) 2003-04-16
KR100643093B1 (ko) 2006-11-10
CN1454284A (zh) 2003-11-05
US7097432B1 (en) 2006-08-29
CN1289791C (zh) 2006-12-13
EP1301689B1 (de) 2006-09-20
JP2004504524A (ja) 2004-02-12
DE60030894T2 (de) 2007-09-06
WO2002006636A1 (fr) 2002-01-24
AU2000267060A1 (en) 2002-01-30

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